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  • Other Sources  (850)
  • ASTRONAUTICS (GENERAL)  (850)
  • 1975-1979  (850)
  • 1900-1904
  • 1
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    In:  CASI
    Publication Date: 2009-11-17
    Description: Principles of rocket engineering, flight dynamics, and trajectories are discussed in this summary of Soviet rocket development and technology. Topics include rocket engine design, propellants, propulsive efficiency, and capabilities required for orbital launch. The design of the RD 107, 108, 119, and 214 rocket engines and their uses in various satellite launches are described. NASA's Saturn 5 and Atlas Agena launch vehicles are used to illustrate the requirements of multistage rockets.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Soviet Aircraft and Rockets (NASA-TT-F-770); p 198-271
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  • 2
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    In:  CASI
    Publication Date: 2006-07-06
    Description: The metallurgical processing experiments on Skylab were chosen to: (1) elucidate the unknown effects of a low gravity environment on certain processes; (2) determine to what extent nongravitational driven flows operate in the processes; and (3) explore the possibilities of containerless solidification. Welding and brazing experiments were conducted to provide an understanding of solidification mechanics in a weightless environment.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 37 p
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  • 3
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    In:  CASI
    Publication Date: 2006-07-06
    Description: A list of the present state of knowledge in materials processing is presented. The fluid behavior in a low gravity environment is summarized. Materials processing in the Space Transportation System facility is discussed. Prospects for space commercialization are reported.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 16 p
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  • 4
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    In:  CASI
    Publication Date: 2006-07-06
    Description: The Apollo Soyuz Test Program is described. A modification of the Skylab furnace was developed for the ASTP mission that had a maximum temperature of 1200 C, a programmed cool down to give more uniform growth rates, and a He quench system to shorten the time required to reach allowable touch temperature. The Space Processing Applications Rocket (SPAR) program was initiated to provide some continuity in flight experimentation. Liquid mixing, immiscible alloy solidification, composite materials, bubbles and dispersed particles during solidification, and containerless processing techniques were studied in the SPAR program.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 45 p
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  • 5
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    In:  CASI
    Publication Date: 2006-07-06
    Description: Several experiments and a number of demonstrations were performed during Skylab to elucidate the behavior of fluids in space. The purposes of these experiments were to confirm hypotheses on how systems would behave in a low-g environment, determine to what extent residual accelerations and nongravity-driven convection affected processes, and provide graphic demonstrations of fluid behavior in space for classroom use and to stimulate new ideas for low-g research.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 33 p
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  • 6
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    In:  CASI
    Publication Date: 2006-07-06
    Description: Numerous applications take advantage of low gravity. These range from research, such as study of basic properties of materials or developing a better understanding of various processes and how they might be controlled, to actual production of unique materials, either in very limited quantities for research purposes to serve as paradigms for determining the limiting results of processes in which gravity effects are removed, or in large quantities, to fill certain high technology needs that cannot be met by other means. Examples of these are given in the following topics discussed: (1) crystal growth; (2) metals, alloys and composite materials (metallurgy); (3) glass and ceramics (containerless processing); (4) fluid and chemical processes; and (5) processing of biological materials.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 60 p
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  • 7
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    In:  CASI
    Publication Date: 2006-07-06
    Description: The following topics are discussed: (1) the inception of space processing; (2) earth-based experimental activities prior to Skylab (drop tower and research aircraft experiments); (3) preliminary experiments in space (Apollo and sounding rocket experiments); and (4) Skylab experimental facilities. Apparatus for contained materials processing; for brazing in space; and containerless processing are presented and discussed. The Skylab materials processing system and miscellaneous design considerations are also discussed.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 48 p
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  • 8
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    In:  CASI
    Publication Date: 2006-06-20
    Description: The materials and processing constraints that are involved in the construction of a molecular wake shield for the shuttle orbiter are discussed. Stainless steel, having outgassing rates less than the required 10 to the minus 12th power Torr-liters/sq cm per second was the primary material suggested for the construction of the shield.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Proc. of Workshops to Define Eng. Requirements for a Space Vacuum Res. Facility; 17 p
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  • 9
    Publication Date: 2006-06-20
    Description: Models depicting the ambient atmosphere which can overtake the spacecraft vacuum shield are presented. The subject areas discussed are: possible changing effects on the wake shield environment; possible utilization of the induced environmental contamination monitor; present state of the knowledge of the parameters used to describe the intermolecular collisions; the possibility of using simple models to describe the wake shield environment; possible errors associated with using kinetic theory to calculate that part of the atmosphere overtaking the shield; and a general assessment of the Monte Carlo techniques used to calculate the shield environment.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Proc. of Workshops to Define Eng. Requirements for a Space Vacuum Res. Facility; 6 p
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  • 10
    Publication Date: 2006-06-20
    Description: Models depicting the collision dynamics in the near vicinity of a body orbiting in the upper atmosphere were studied to investigate degassing techniques for a vacuum facility.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Proc. of Workshops to Define Eng. Requirements for a Space Vacuum Res. Facility; 3 p
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  • 11
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    In:  CASI
    Publication Date: 2006-04-10
    Description: The selection of biological products was studied for electrophoresis in space. Free flow electrophoresis, isoelectric focusing, and isotachophoresis are described. The candidates discussed include: immunoglobulins and gamma globulins; isolated islet of langerhans from pancreas; bone marrow; tumor cells; kidney cells, cryoprecipitate; and column separated cultures.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 177-190
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  • 12
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    In:  CASI
    Publication Date: 2006-04-10
    Description: High purity tungsten, which is used for targets in X-ray tubes was considered for space processing. The demand for X-ray tubes was calculated using the growth rates for dental and medical X-ray machines. It is concluded that the cost benefits are uncertain.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 159-176
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  • 13
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    In:  CASI
    Publication Date: 2006-04-10
    Description: The potential demand for space processed turbine blades, and the dollar benefits to be derived from this technology were analyzed. It was found that an adequate demand to justify space processed blades will exist. The cost benefits per blade for replacements in existing aircraft is estimated to be $997.50 per blade, and for new aircraft the savings per blade would be over $21,000.00.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 40-90
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  • 14
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    In:  CASI
    Publication Date: 2006-01-16
    Description: A major goal of Skylab was to learn more about man and his responses to the space environment for missions lasting up to 84 days. A review of Skylab data pertaining to this goal is given.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Biomed. Results from Skylab; p 408-418
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  • 15
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    In:  CASI
    Publication Date: 2006-01-16
    Description: The entire field of rocketry and astronautics in Spain was studied. Congreve war rockets in military actions were emphasized in the African war, the Cuban campaign and the Spanish Civil War. Rockets in space travel were also summarized along with space science fiction.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA, Washington Essays on the History of Rocketry and Astronautics, Vol. 1; p 78-101
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  • 16
    Publication Date: 2006-01-16
    Description: The work of a Soviet scientist and inventor of the 19th century, S. S. Nezhdanovsky, is discussed. Investigations in the field of aircraft science and technology are emphasized in relation to Nezhdanovsky's studies of using the jet principle in solving the problem of human flight. Nezhdanovsky dealt with calculations of the speed at which combustion products flow, and considered such problems as fuel feeding into the combustion chamber by means of pumps, and the use of one of the fuel components for cooling the walls of the combustion chamber.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA, Washington Essays on the History of Rocketry and Astronautics, Vol. 1; p 125-139
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  • 17
    Publication Date: 2006-01-16
    Description: The development of rocket technology in Poland is outlined. The history cites 13th century use of war rockets in combating Tartars as well as 20th century studies of the future and reality of space flights.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA, Washington Essays on the History of Rocketry and Astronautics, Vol. 1; p 102-111
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  • 18
    Publication Date: 2006-01-16
    Description: A study of rocket dynamics done by K. E. Tsiolkovsky in 1896 is reported. Problems in rectilinear movement of rockets were studied. Calculations were done on velocity efficiency, motion in free space, motion in a homogeneous gravitational field and motion with constant acceleration.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA, Washington Essays on the History of Rocketry and Astronautics, Vol. 1; p 115-124
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  • 19
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    In:  CASI
    Publication Date: 2006-01-12
    Description: The problem of physical crowding and the proliferation of separate communication links and ground support systems for multiple free-flying satellites can be overcome by using space platforms and multiplexing the data streams. Pertinent features of the space shuttle orbiter payloads, the solar power satellite, and geostationary and geosynchronous platforms are discussed. Typical payload requirements data which are needed to allow meaningful study of payloads as candidates for platform implementation are cited and factors affecting the compatibility/grouping of payloads are outlined.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Proc.: Workshop on the Need for Lightning Observations from Space; p 159-182
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  • 20
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    In:  CASI
    Publication Date: 2006-01-16
    Description: The works of Guido von Pirquet, Austrian pioneer of rocketry, were assessed. Major emphasis was given to Pirquet's calculation of the route to Venus which in fact was followed by the first Russian rocket to Venus. Of interest also is Pirquet's valuable construction of a space station and his analysis of interstellar space flight.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA, Washington Essays on the History of Rocketry and Astronautics, Vol. 1; p 140-155
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  • 21
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    In:  CASI
    Publication Date: 2006-01-16
    Description: Progress on Project Mercury, program for manned orbital space flight, is briefly reviewed. The original aims and concepts of the project are recounted. Various types of launch apparatus are mentioned along with safety factors.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Collected Works of Charles J. Donlan; 6 p
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  • 22
    Publication Date: 2006-01-16
    Description: A very broad mission objective was established; i.e., manned circumlunar flight and return to earth. It is implicit that the Saturn will be the primary propulsion system for this mission. The following attempts to: (1) define the objective so as to achieve as much capability in the vehicle as possible; (2) draw on Mercury experience to provide broad guidelines for vehicle performance and safety; (3) provide flexibility in the vehicle capability in the event that the manned lunar mission is proved to be subject to unacceptable risk in the target time period; and (4) indicate problem areas where work appears to be particularly needed.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Collected Works of Charles J. Donlan; 66 p
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  • 23
    Publication Date: 2006-01-12
    Description: The suitability of existing terrestrial extractive metallurgical processes for the production of Al, Ti, Fe, Mg, and O2 from nonterrestrial resources is examined from both thermodynamic and kinetic points of view. Carbochlorination of lunar anorthite concentrate in conjunction with Alcoa electrolysis process for Al; carbochlorination of lunar ilmenite concentrate followed by Ca reduction of TiO2; and subsequent reduction of Fe2O3 by H2 for Ti and Fe, respectively, are suggested. Silicothermic reduction of olivine concentrate was found to be attractive for the extraction of Mg becaue of the technological knowhow of the process. Aluminothermic reduction of olivine is the other possible alternative for the production of magnesium. The large quantities of carbon monoxide generated in the metal extraction processes can be used to recover carbon and oxygen by a combination of the following methods: (1) simple disproportionation of CO,(2) methanation of CO and electrolysis of H2O, and (3) solid-state electrolysis of gas mixtures containing CO, CO2, and H2O. The research needed for the adoption of earth-based extraction processes for lunar and asteroidal minerals is outlined.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Ames Res. Center Space Resources and Space Settlements; p 257-274
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  • 24
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    In:  CASI
    Publication Date: 2006-01-12
    Description: The first lunar supply base should have a mass less than 1000 tons, be deployed by 24 persons in 4 months, and be maintained by 10 persons. Output could be expanded 20 times in 5 years to 600,000 tons/yr by a factor of 10 expansion of the area of the solar array on the lunar surface, using low power soil beneficiation, increasing the fleet of mining vehicles, and illuminating the base continuously at night with lunar orbiting mirrors. The space manufacturing facility (SMF) will supply most of the mass (solar cells and orbiting mirrors) necessary for expansion. Several devices and procedures are suggested for development which could further reduce the total mass necessary to transport to the Moon to establish the initial lunar supply base.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Ames Res. Center. Space Resources and Space Settlements; p 207-224
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  • 25
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    In:  CASI
    Publication Date: 2006-01-12
    Description: Solidification of magnetic materials in the low gravity orbital environment was studied. The magnetic compounds under study, manganese bismuth and copper cobalt cerium ((Cu, Co)5Ce), both have the potential for the development of high coercive strength. Preliminary results indicate that static fluid configurations, in the absence of the gravitational body force, differ substantially from the documented terrestrial behavior. Chemical homogeneity is substantially enhanced on a macroscopic and microscopic level. Single crystal matrices have been grown in the coordinated growth regions of the flight samples. Primary crystals one order of magnitude greater than those grown terrestrially have been noted and are limited in size by the ampoule dimensions.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Lyndon B. Johnson Space Center Apollo-Soyuz Test Project; 13 p
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  • 26
    Publication Date: 2006-01-16
    Description: Estimates of short and long term solar activity are required for calculating variations in the environment with regard to spacecraft charging, radiation effects, and orbital lifetime. Correlations appear to exist between the time of solar activity and the time of operational anomalies due to electrical discharges when the dielectric surfaces of geosynchronous spacecraft are charged by interaction with the ambient plasma to levels above breakdown voltage. An ability to predict the solar induced variation variability of the plasmas could permit refinement of design criteria. The influence of the radiation on spacecraft materials, systems, and manned operations is summarized. Solar radition effects on the orbital altitude atmospheric density environment and spacecraft lifetimes are also considered.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Solar-Terrest. Predictions Proc., Vol. 2; p 89-103
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  • 27
    Publication Date: 2006-01-16
    Description: Areas which are influenced by solar-terrestrial coupling effects and which are internal to the Earth's magnetosphere are of interest to mission planners, spacecraft hardware designers, and those engaged in the operation of already orbiting manned or unmanned spacecraft. Accurate models are needed to predict energetic particle flux density, interactions between low energy (10 eV to 100 eV) near-Earth plasma and space systems, and neutral atmospheres. Parameters required for each of these areas are discussed.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Solar-Terrest. Predictions Proc., Vol. 2; p 1-20
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  • 28
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    In:  CASI
    Publication Date: 2006-04-10
    Description: An econometric model was developed that can be used to predict demand and supply figures for crystals over a time horizon roughly concurrent with that of NASA's Space Shuttle Program - that is, 1975 through 1990. The model includes an equation to predict the impact on investment in the crystal-growing industry. Actually, two models are presented. The first is a theoretical model which follows rather strictly the standard theoretical economic concepts involved in supply and demand analysis, and a modified version of the model was developed which, though not quite as theoretically sound, was testable utilizing existing data sources.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 191-233
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  • 29
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    In:  CASI
    Publication Date: 2006-04-10
    Description: Space processing of directionally solidified eutectic-alloy type turbine blades is envisioned as a simple remelt operations in which precast blades are remelted in a preformed mold. Process systems based on induction melting, continuous resistance furnaces, and batch resistance furnaces were evaluated. The batch resistance furnace type process using a multiblade mold is considered to offer the best possibility for turbine blade processing.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 91-158
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  • 30
    Publication Date: 2006-01-12
    Description: A conceptual design is presented for fiberglass production systems in both lunar and space environments. The raw material, of lunar origin, will be plagioclase concentrate, high silica content slag, and calcium oxide. Glass will be melted by solar energy. The multifurnace in the lunar plant and the spinning cylinder in the space plant are unique design features. Furnace design appears to be the most critical element in optimizing system performance. A conservative estimate of the total power generated by solar concentrators is 1880 kW; the mass of both plants is 120 tons. The systems will reproduce about 90 times their total mass in fiberglass in 1 year. A new design concept would be necessary if glass rods were produced in space.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Ames Res. Center Space Resources and Space Settlements; p 225-232
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  • 31
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    In:  CASI
    Publication Date: 2006-01-11
    Description: Operating principles, system functions, and technological problems associated with developing compatible spacecraft, station approach, and docking facilities between the U.S. and the U.S.S.R. are reported. Two designs, the probe cone and the androgynous docking device are examined.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Mod. Achievements of Cosmonautics (NASA-TT-F-16221); p 20-38
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  • 32
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    In:  CASI
    Publication Date: 2006-07-06
    Description: Five experiments involving the processing of semiconductor materials were performed during the Skylab mission. After discussions on semiconductors and their unique electronic properties, and techniques of crystal growth, these five experiments are presented. Four melt growth experiments were attempted: (1) steady state growth and segregation under zero gravity (InSb); (2) seeded, containerless solidification of InSb; (3) influence of gravity-free solidification on microsegregation; and (4) directional solidification of InSb-GaSb alloys. One vapor growth experiment, crystal growth by vapor transport, was attempted.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 45 p
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  • 33
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    In:  CASI
    Publication Date: 2006-07-06
    Description: The long exposure to a virtually zero-gravity environment is a truly unique situation that cannot be duplicated or even approximated for any length of time on earth. The topics discussed are: (1) low gravity; (2) atmospheric effects; (3) potential advantages of materials processing in space; (4) the absence of buoyancy-driven convection; (5) the absence of hydrostatic pressure; (6) the absence of sedimentation and buoyancy; (7) containerless processing; and (8) ultrahigh vacuum processing.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Early Space Expt. in Mater. Process.; 37 p
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  • 34
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    In:  CASI
    Publication Date: 2006-04-10
    Description: An economic analysis using econometric and cost benefit analysis techniques was performed to determine the feasibility of space processing of certain products. The overall objectives of the analysis were (1) to determine specific products or processes uniquely connected with space manufacturing, (2) to select a specific product or process from each of the areas of semiconductors, metals, and biochemicals, and (3) to determine the overall price/cost structure of each product or process considered. The economic elements of the analysis involved a generalized decision making format for analyzing space manufacturing, a comparative cost study of the selected processes in space vs. earth manufacturing, and a supply and demand study of the economic relationships of one of the manufacturing processes. Space processing concepts were explored. The first involved the use of the shuttle as the factory with all operations performed during individual flights. The second concept involved a permanent unmanned space factory which would be launched separately. The shuttle in this case would be used only for maintenance and refurbishment. Finally, some consideration was given to a permanent manned space factory.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 234-251
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  • 35
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    In:  CASI
    Publication Date: 2006-04-10
    Description: Space processing concepts investigated included an unmanned space factory, and a permanently launched factory. Product lines chosen for analysis were: (1) turbine blades, (2) tungsten targets for X-ray machines, (3) 1 sub G subclass separation by electrophoresis, and (4) high-price exotic crystals. The turbine blade, and 1 sub G products are considered promising candidates.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Econ. Analysis of Materials Processing in Space; p 1-7
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  • 36
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    In:  Other Sources
    Publication Date: 2011-08-16
    Description: Factors affecting crew performances in long-term space flights are examined with emphasis on the Space Shuttle-Spacelab program. Biomedical investigations carried out during four Skylab missions indicate that initially rapid changes in certain physiological parameters, notably in cardiovascular response and red-blood-cell levels, lead to an adapted condition. Calcium loss remains a potential problem. Space Shuttle environmental control and life-support systems are described together with technology facilitating performance of mission objectives in a weightless environment. It is concluded that crew requirements are within the physical and psychological capability of astronauts, but the extent to which nonastronaut personnel will be able to participate without extensive training and pre-conditioning remains to be determined.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 13; Oct. 197
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  • 37
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    Publication Date: 2011-08-16
    Description: Studies evaluating potential operational and commercial uses of space are being conducted, taking into account astronomy, astrophysics, manned bases and laboratories in earth orbit, space colonization, terrestrial communications, space processing and manufacturing, interstellar probes, planetary exploration, and the use of space for terrestrial energy supply. The present status in the exploration of the solar system is examined, giving attention to Jupiter, Venus, Mars, and Mercury. A brief outline of the development of human colonies on Mars is presented.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Spaceflight; 17; Mar. 197
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  • 38
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    Publication Date: 2011-08-16
    Description: The effort performed to assure proper flight program handling of time bases, discretes, and interrupts was discussed. The following time bases are used as key mission events: guidance reference release, liftoff, S-1B low level sensors dry, S-1B outboard engines cutoff, S-IVB cutoff, and S-IVB de-orbit DCS command. The five discrete outputs in the discrete output register were verified for proper setting. Each discrete input is honored in the proper time frame by forcing each discrete in the following intervals: before the discrete is enabled, after the discrete has been detected, and after the discrete has been disabled. As an assurance that an interrupt is honored only in the proper time frames, each interrupt was forced during the following intervals: prior to the specified enable time, after the interrupt has been honored, after the interrupt has been disabled.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Program Verification Doc. for the ASTP Flight Program; 10 p
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  • 39
    Publication Date: 2011-08-17
    Description: Contaminating fluxes from upper atmospheric molecules found in the wake of a typical spacecraft of the Long Duration Exposure Facility class are studied with the aim of determining vacuum levels which may be employed by experiments mounted on the vehicle. A simplified representation for the spacecraft, the velocity-shifted Maxwellian distribution (to evaluate ambient flux which has a velocity sufficient to overtake the spacecraft), and a calculation for the backscattered contribution to the flux density of the wake figure in the study are presented. Results indicate that direct and backscattered fluxes of about 10 to the seventh power molecules per sq cm can be expected in the wake of a spacecraft at 550 km altitude.
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  • 40
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    Publication Date: 2011-08-17
    Description: The composition of the atmosphere within the planned orbital envelope of the Space Shuttle and the velocity necessary to maintain a stable orbit within that envelope provide unique conditions for forming a high-purity, moderate energy beam (about 5 eV) of atomic oxygen. At 500 km, for example, atomic oxygen comprises approximately 90% of the atmosphere. Since the mean thermal speed of the ambient atomic oxygen is substantially less than the orbital speed, a high-purity beam can be generated by sweeping through the gas with a series of beam-forming truncated conical shells. Characteristics of the beam, including energy distribution, flux, and purity variation with orbital altitude and methods for lowering the mean energy, are presented. Gas-surface interaction experiments that have been proposed for this laboratory are also discussed.
    Keywords: ASTRONAUTICS (GENERAL)
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  • 41
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    Publication Date: 2011-08-17
    Description: Manned spaceflight is considered within the framework of two broad categories: human exploitation of space for economic or scientific gain, and human habitation of space as a place where man may live, grow, and actualize himself. With the advent of the Space Shuttle, exploitation of space will take the form of new product development. This will continue during the 1990s as the new products are manufactured on a scale large enough to be profitable. The turn of the century should see major industries in space, and large space habitats. Thus, the question of mankind's existential needs arises. In addition to basic physical needs, the spiritual and cultural requirements of human beings must be considered. The impact of man's presence in space upon human culture in general is discussed with reference to international cooperation, public interest in space programs, scientific advancement, the basic urge to explore, and the density of mankind as a whole; which will become free of external constraints as we step into the cosmos.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Spaceflight; 20; Feb. 197
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  • 42
    Publication Date: 2011-08-17
    Description: The International Sun-Earth Explorer (ISEE) is a three-spacecraft system developed by NASA and ESA to study the magnetospheric structure, paying attention to the quantitative mechanism of magnetospheric response to external perturbations, and the structure of its parts. In particular, the nature, structure, motion, and stability of magnetospheric boundaries will be studied, including bow shock, magnetopause, plasmapause, and neutral sheet. Spacecraft ISEE-A and ISEE-B will be launched into the same orbit (of apogee 23 earth radii) but separated by a small, controllable distance, and will make observations from within the magnetosphere. The ISEE-C spacecraft will be launched into a heliocentric orbit (234 earth radii upstream) and will make observations in the solar wind upstream of the earth.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Science; 198; Oct. 14
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  • 43
    Publication Date: 2011-08-17
    Keywords: ASTRONAUTICS (GENERAL)
    Type: CNES Technol. of Sci. Space Expt.,; p 119-134
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  • 44
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    Publication Date: 2011-08-17
    Description: The project development and active flight of the Mariner 10 deep-space probe mission is recounted in detail, with sequential blow-by-blow coverage. Early studies and speculation on the planet Mercury are reviewed, and the spin-orbit coupling and near-synchronous rotation of the planet are described. Use of Venus as a slingshot in a gravity-assist maneuver is described, and Mariner 10 records of Venus are shown. The three encounters of Mariner 10 with Mercury (March 1974, Aug. 1974, March 1975) are described in detail, with purposes, problems, mishaps, and glossy photographs recovered from Mariner 10 data. Information on the planet's magnetosphere, surface topography, inferred internal structure, and IR signature is provided, and the end-of-mission improvised solar-sail experiment is outlined.
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  • 45
    Publication Date: 2011-08-17
    Description: The results reached by the DSN engineering section and private consultants in the review of the initial plan of the Golstone Energy Project are summarized. The main objectives were in the areas of energy conservation and the application of solar-driven systems for power and hydrogen generation. This summary will provide background data for management planning decisions both to the DSN engineering section and other organizations planning a similar program. The review showed that an add-on solar driven absorption refrigeration unit with its associated changes to the existing system was not cost-effective, having a payback period of 29 years. Similar economically unattractive results were found for both a solar-hydrogen and a wind-hydrogen generation plant. However, cutting the hydrogen generation linkage from this plant improved its economic feasibility.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: The Deep Space Network; p 120-140
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  • 46
    Publication Date: 2011-08-17
    Description: An experiment on melting and directional crystallization of an antimony (Sb) doped germanium silicon (GeSi) solid solution was designed for the Apollo-Soyuz Test Project (ASTP) to study the possibility of using zero-g conditions for obtaining solid-solution monocrystals with uniformly distributed components. Crystallization in the zero-g environment did not occur under ideal stationary growth and segregation conditions. Crystallization under zero-g conditions revealed the heterogeneous nature of Si and Sb distribution in the cross sections of crystals. The presence of the radial thermal gradient in the multipurpose furnace could be one of the reasons for such Si and Sb distribution. The structure of space-grown crystals correlates with the nature of heterogeneities of Si and Sb distribution in crystals. The type of surface morphology and the contour observed in space-grown crystals were never observed in ground-based crystals and indicate the absence of wetting of the graphitized walls of the ampoule by the melt during melting and crystallization.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Apollo-Soyuz Test Project (date]; 36 p
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  • 47
    Publication Date: 2011-08-17
    Description: The experiment was designed to detect possible convection caused by a steplike compositional variation in a liquid metal in a microgravity environment. Wetting and nonwetting ampoules were used to try to determine the extent of the stirring effects if they were present. Since stirring effects can be caused by temperature gradients, the temperature gradients were minimized. Steplike compositional variation was created by pressure bonding a lead-0.05 atom percent gold alloy to pure lead. Two diffusion temperatures (923 K and 723 K) were used; if no stirring effects were present, it was hoped that the liquid diffusion parameters for gold in lead could be obtained. Two identifical experimental arrangements were used to compare the transport mechanisms of gold in liquid lead in unit gravity and microgravity environments.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Apollo-Soyuz Test Project; 87 p
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  • 48
    Publication Date: 2011-08-16
    Description: A summary is presented of NASA's activity in materials research in zero-g. Very simple experiments to determine the effects of zero-g upon solidification processes, upon heat flow, convection and mass transport, and upon the separation of biological cells were conducted during three Apollo flights. The investigations were continued in a series of experiments conducted on Skylab. The experiments provided data on a wide range of space-processing topics. The various tests and the results obtained in them are discussed. Attention is also given to experiments planned for the Apollo-Soyuz experiment, studies to be conducted with the aid of sounding rockets, and an evaluation of the possibilities provided by space processing for industry.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 13; May 1975
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  • 49
    Publication Date: 2011-08-16
    Description: A technique has been developed to obtain a characterization of the self-generated environment of a spacecraft and its variation with time, angular position, and distance. The density, pressure, outgassing flux, total weight loss, and other important parameters were obtained from data provided by two mass measuring crystal microbalances, mounted back to back, at a distance of 1 m from the spacecraft equivalent surface. The strongest source appeared to be caused by a material diffusion process which produced a directional density at 1 m distance of about 160 billion molecules per cu cm after 1 h in vacuum and decayed to 1.6 billion molecules per cu cm after 200 h. Self-contamination of the spacecraft was equivalent to that which occurs in a 300-km altitude orbit.
    Keywords: ASTRONAUTICS (GENERAL)
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  • 50
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    Publication Date: 2011-08-16
    Description: The verification accomplished to assure correct computation of the many geometrical relationships between the several coordinate systems and transformation matrices defined for the Saturn 1B mission was discussed. This is accomplished by demonstrating the following: (1) the program has the ability to correctly establish the initial vector coordinate system from external input data for use as a reference, (2) the program logic is capable of properly executing the calculations necessary to transform vectorial parameters from one coordinate system to another, and (3) the presettings used for vector component calculations are valid.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Program Verification Doc. for the ASTP Flight Program; 3 p
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  • 51
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    Publication Date: 2011-08-16
    Description: A brief general description of the ASTP flight program verification was presented. The total program verification effort assures the accuracy and adequacy of the LVDC flight program and verifies that the final program meets mission requirements and conforms to program documentation. The flight program's functional requirements to integrate the guidance and control system with the launch vehicle sequencing system are verified directly by analysis of many special logic checks designed for this purpose and indirectly by the correct overall program response to nominal and numerous perturbed conditions. Verification of the interaction of function requirements is accomplished on every case run during the verification effort.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Program Verification Doc. for the ASTP Flight Program; 3 p
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  • 52
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    Publication Date: 2011-08-16
    Description: A communications system for performing the basic functions of mission operations, orbit and attitude determination, and data processing is described. A block diagram is provided to show the relationships of these functions with the spacecraft in orbit and the experiments to be conducted on board the spacecraft. Specific areas of application are discussed as follows: (1) software operating systems for the ATS-F satellite testing and ground support, (2) inversion of the RAE-1 satellite (Explorer 38 satellite) in orbit, (3) ALSEP differential Doppler tracking, (4) minitrack calibration using satellite data, (5) angles-only orbit extraction, and (6) image processing system performance prediction and product quality evaluation techniques. Block diagrams of the various systems are provided to show the steps involved in the operations.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Significant Accomplishments in Sci. and Technol.; p 290-319
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  • 53
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    Publication Date: 2011-08-17
    Description: Future possibilities for the further study of the asteroids are reviewed, with particular attention paid to space missions for their direct exploration. The role of traditional ground-based and earth orbiting techniques is examined briefly, and it is concluded that although astronomical techniques are presently at their peak, and despite the opportunities provided by the Infrared Astronomical satellite, the Space Telescope and Spacelab Infrared Telescope Facility, the next major step will require direct exploration by space probes to obtain information on asteroid surface chemistry, geology and bulk properties. Various mission modes and propulsion systems for a first multi-target asteroid mission are discussed, including flyby, rendezvous, landing and sample return, and ion-drive propulsion systems. Science payloads for a basic rendezvous mission are considered, and target selection for multi-asteroid flyby tours and rendezvous tours is discussed. Consideration is also given to sample return missions for the evaluation of the asteroid as potential resources.
    Keywords: ASTRONAUTICS (GENERAL)
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  • 54
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    Publication Date: 2011-08-18
    Description: Some physical and chemical processes involved in the evaporation and sublimation of mixtures of frozen gases are discussed. Effects of zero gravity, vacuum, and solar radiation are emphasized. Relevant experiments that can be carried out with the aid of the space shuttle are proposed.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Proc. of the Shuttle-Based Cometary Sci. Workshop; p 137-141
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  • 55
    Publication Date: 2011-08-18
    Description: It is proposed to use the Shuttle (OFT experiments) or eventually Spacelab to study, in the absence of gravity the low velocity accretion and the bulk properties of icy conglomerates simulating cometary material and their sedimentation and bulk properties in very small acceleration fields. Their behavior when exposed to the direct solar flux is also under consideration.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Proc. of the Shuttle-Based Cometary Sci. Workshop; p 99-117
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  • 56
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    Publication Date: 2011-08-18
    Description: The different modes of cometary investigation offered by the shuttle are reviewed. First, there is a mode in which instrumentation for observations of a natural comet is carried to orbit on Spacelab. Second is a mode in which gaseous or solid material is released from the shuttle to simulate some aspect of cometary physics. Another mode uses the near weightlessness within Spacelab to allow laboratory experiments with materials as they may exist on the surface of a comet nucleus.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Proc. of the Shuttle-Based Cometary Sci. Workshop; p 5-6
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  • 57
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    Publication Date: 2011-08-18
    Description: A continuing source of difficulty in cometary astrophysics is understanding the origin of C2, C3, NH and CO(+) species in comets. An experiment is proposed to investigate these problems by continuously releasing suspected parent gases from the space shuttle and using a dye laser to selectively excite fragments produced as a result of solar photochemical decomposition of the molecules. The backscattered fluorescence is gathered by a telescope, spectrally filtered, and measured as a function of time after the laser pulse.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Proc. of the Shuttle-Based Cometary Sci. Workshop; p 118-136
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  • 58
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    Publication Date: 2011-08-18
    Description: The experiments considered are in two groups: on-board experiments and overboard experiments. The on-board experiments include the determination of bulk properties and processes (within solids) and observations of exposure panels (near surface phenomena) The overboard experiments consist of analysis of gas/dust shells by observation from the shuttle and observation by sub-satellites. Experimental parameters are discussed with emphasis on work that is unique to low gravity and high vacuum environments.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Proc. of the Shuttle-Based Cometary Sci. Workshop; p 160-166
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  • 59
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    Publication Date: 2011-08-17
    Description: The weightless environment onboard spacecraft in drifting flight has provided a unique opportunity to do experiments that cannot be done on the ground. High resolution free-fluid electrophoresis of particles proposed in the late 1960s to take advantage of reduced gravity began with brief experiments done during two Apollo flights. The recent Apollo Soyuz Test Project mission had two major experiments that accomplished the separation of viable biological cells. Experiments now are being planned for the Space Shuttle which will attempt to achieve high resolution of the separated species by using zone electrophoresis. These experiments will return a quantity sufficient for laboratory testing and establish the potential of fractionation and purification of biological materials in space.
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  • 60
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    Publication Date: 2011-08-17
    Description: Experiments to study the dynamics of liquid drops are being planned to be performed in the weightless environment of Spacelab. The liquids will range from superfluid helium through ordinary liquid to molten metals and glasses. The experiments will be conducted in a chamber now being developed which utilizes the forces and torques produced by acoustic waves excited within the chamber. None of the currently available facilities (drop towers, sounding rockets, or zero-g aircraft flights) can provide a sustained weightless environment, since the resulting zero-g periods are from 3 sec to 5 min. Spaceflight, however, will provide weightlessness for periods of one week, or more, allowing truly laboratory-like experiments to be conducted on free liquid drops and bubbles. In this paper we discuss both the drop dynamics experiments proposed for Spacelab and the acoustic chamber: its operation and current testing for these and other experiments.
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  • 61
    Publication Date: 2011-08-17
    Description: Experiment MA-060 was designed to establish the crystal growth and segregation characteristics of a melt in a directional solidification configuration under near zero-g conditions. The interface demarcation technique was incorporated into the experiment since it constitutes a unique tool for recording the morphology of the growth rate throughout solidification, and for establishing an absolute time reference framework for all stages of the solidification process. An extensive study was performed of the germanium crystals grown during the Apollo-Soyuz Test Project mission. It was found that single crystal growth was achieved and that the interface demarcation functioned successfully. There was no indication that convection driven by thermal or surface tension gradients was present in the melt. The gallium segregation, in the absence of gravity, was found to be fundamentally different in its initial and its subsequent stages from that of the ground-based tests. None of the existing theoretical models for growth and segregation can account for the observed segregation behavior in the absence of gravity.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Apollo-Soyuz Test Project; 65 p
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  • 62
    Publication Date: 2011-08-17
    Description: The purpose of experiment MA-060 was to investigate quantitatively the effects of near-zero gravity conditions on crystal growth and dopant segregation during directional solidification from the melt. Gallium-doped germanium single crystals were successfully grown from the melt with simultaneous interface demarcation during the Apollo Soyuz Test Project mission. The analysis of the experimental data indicates striking differences of dopant segregation and growth behavior in the presence and absence of gravity. The results obtained are believed to have far-reaching implications on materials processing under zero-gravity conditions and on the theory of crystal growth and segregation in general.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: ESA Mater. Sci. in Space; p 181-187
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  • 63
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    Publication Date: 2011-08-17
    Description: An overview is given of the definition of research requirements and derivation of engineering design requirements for a group of 77 representative applications of space processing. Representative requirements are documented for applied research in space on biological processes, chemical/fluid phenomena, solidification processes, and glass/ceramics processes. Design requirements for payload equipment to accommodate these research requirements are presented in engineering terms, such as power requirements, schematic diagrams, etc. In addition, a summary of the 77 applied research topics is included.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: ESA Mater. Sci. in Space; p 87-113
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  • 64
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    Publication Date: 2011-08-17
    Description: The processing of materials in a low-g environment was started approximately 10 years ago. This article surveys the apparatus developed during that period. A low-g environment occurs naturally in a free-flying spacecraft (e.g., in manned flights such as Apollo, Skylab, and ASTP); low-g conditions also occur in other free-falling bodies such as sounding rockets and drop tower capsules. Apparatus has been developed for all these craft. Most of the apparatus described serves to melt and resolidify materials in low g; the material may be contained or, by virtue of the environment, freely floating. Other apparatus for separation of intimately mixed components or species is also described. A general conclusion is drawn that the apparatus addresses only a few of the possibilities available, is still at the experimental stage, and is of laboratory scale. It is predicted that processes showing promise will be scaled up to derive economic advantages in the Shuttle era of space flight.
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  • 65
    Publication Date: 2011-08-17
    Description: A saturated solution of NH4Cl was solidified on earth at 1 g and in a suborbital rocket flight at .00001 g. In the 1 g experiments, macrosegregation caused by the gravitational acceleration was marked. Nucleation started at the cold walls after which dendrites and dendritic debris were swept into the center of the cuvette by convective fluid flow. Secondary dendrite arms were oriented toward the cold wall. When solidified in low g, only four nuclei grew to form the complete casting. There were no free floating crystals or visible dendrite remelting. The lack of fluid flow allowed symmetrical dendrite growth into the fluid.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Metallurgical Transactions A - Physical Metallurgy and Materials Science; 8A; Jan. 197
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  • 66
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    Publication Date: 2011-08-17
    Description: The Apollo program was designed to land men on the moon and return them safely to earth. The Apollo lunar missions were informally divided into series, each series having similar spacecraft configurations, number of experiments, and complexity of tasks. Specific information on these missions is given.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Catalog of Lunar Mission Data; p 55-149
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  • 67
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    Publication Date: 2011-08-17
    Description: The Luna and Zond series of unmanned U.S.S.R. spacecraft were designed to investigate the moon and its vicinity. Sixteen Luna spacecraft and, six Zond spacecraft have obtained lunar data. These series have included flyby, lunar-orbiting, and soft-landing missions. A variety of experiments were carried out by these spacecraft including studies of magnetism, X-ray and gamma emissions, gravitational anomalies, and chemical composition. Soil samples, near- and farside photography (both color and black and white), and earth-cloud photography were also acquired. Luna 17 and 23, carried automatic roving vehicles (Lunokhod 1 and 2) that traversed portions of the lunar surface. Lunokhod 1 roamed in Mare Imbrium near Sinus Iridum, and Lunokhod 2 roamed in the Crater Le Monnier at the eastern edge of Mare Serenitatis. The Luna 16, 20, and 24 missions soft-landed on the lunar surface, scooped up lunar material, and returned these samples to earth. The photographic samples received are in the form of paper prints. Some publications containing photographs are described.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Catalog of Lunar Mission Data; p 39-51
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  • 68
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    Publication Date: 2011-08-17
    Description: The Surveyor program consisted of seven unmanned lunar missions. Five of these spacecraft, Surveyor 1, 3, 5, 6, and 7, successfully soft-landed on the lunar surface. These missions and the resulting data are discussed. In addition to demonstrating the feasibility of lunar surface landings, the Surveyor missions obtained lunar and cislunar photographs and both scientific and technological information needed for the Apollo manned landing program. Four spacecraft, Surveyor 1, 3, 5, and 6, returned data from selected mare sites for Apollo program support, and Surveyor 7 provided data from a contrasting rugged highland region.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Catalog of Lunar Mission Data; p 19-35
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  • 69
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    Publication Date: 2011-08-17
    Description: The flight test furnace run of the monotectic and syntectic alloys experiment was successfully performed during the Apollo-Soyuz Test Project mission in July 1975. Examination of the returned sample cartridges and the formal comparative characterization of the low-g and one-g processed samples of lead-zinc and aluminum antimonide were completed. The results for aluminum antimonide show that polycrystalline and multiphased material can be homogenize in space under low-g conditions. Microstructural study on the lead-zinc flight samples shows that complete interdiffusion of lead and zinc had not been achieved, even though the flight data indicated a soak temperature in the miscible region that was 40 K above the published consolute temperature.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Apollo-Soyuz Test Project; 51 p
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  • 70
    Publication Date: 2011-08-17
    Description: The positive effects of microgravity on crystal quality and fundamental properties of the vapor transport reaction were established by analyzing the results of three transport experiments on multi-component systems performed during the Apollo Soyuz Test Project (ASTP) mission. The systems employed were GeSe(0.99)Te(0.01) - GeI4 (A), GeS(0.98)Se(0.02) - GeCl4 (B), and GeS - GeCl4-Ar (C). The crystallographic analysis is based on a direct comparison of space and ground-based (prototype) crystals, employing X-ray diffraction, microprobe, microscopic, and chemical etching techniques. The results demonstrate a considerable improvement of the space-grown crystals in terms of chemical and crystalline homogeneity, surface morphology, and bulk perfection relative to ground specimens. The confirmation of greater mass transport rates than predicted for micro-gravity by present vapor transport models is of basic scientific and practical importance for the improvement of transport models and techniques on earth and for the development of a transport model for space conditions. The internal consistency and agreement between ASTP and Skylab results obtained for different compounds, transport agents, and temperature gradients strongly support the validity of these observations. The combined findings of improved crystal quality and high mass transport rates are of technological significance for space-processing applications.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: ESA Mater. Sci. in Space; p 189-206
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  • 71
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    Publication Date: 2011-08-17
    Description: A general overview of materials experiments done on several Apollo missions and Skylab as well as the ground research that led to these experiments is given. Demonstrations of composite solidification, electrophoresis, and fluid flow were developed for Apollo. Fourteen different experiments in metal processing and single crystal growth were done in the space processing facility on Skylab. Metals were melted and solidified in a variety of configurations using different methods of heating to produce improved alloys and composite materials. Single crystals were grown by directional solidification and vapor transport to achieve uniform crystalline perfection, decreased structural defects, and homogeneity of the dopant material.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: ESA Mater. Sci. in Space; p 19-26
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  • 72
    Publication Date: 2011-08-16
    Description: Analysis of a molecular shield orbited at 200 km utilizes the kinetic theory of a drifting Maxwellian gas, applied to a hemispherical shell geometry containing internal sources. The molecular shield provides very low gas density conditions for materials experiments at low gravity, while the hemispherical geometry minimizes the internal surface/volume ratio. Deployment of the shield in orbit is described. Contributions to density by shield outgassing, by experiment outgassing, and by interaction with the orbiter are discussed separately. A jettisonable closure plate sealing the hemisphere minimizes any risk of experiment contamination during deployment.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Journal of Vacuum Science and Technology; 13; May-June
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  • 73
    Publication Date: 2011-08-16
    Description: NASA planning aspects of potential future manned space flight missions are examined and the necessity of long-range planning is pointed out. A listing of desirable future activities is considered, taking into account the permanent occupancy of near-earth orbit space, the permanent occupancy of earth-moon space, the full self-sufficiency of man in geolunar space, and the permanent occupancy of heliocentric space. The technological requirements for the considered activities are discussed, giving attention to transportation, habitation, engineering technology, life sciences, operations technology, and advanced management concepts. A description of future program phasing and advanced studies requirements is also given.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: British Interplanetary Society; vol. 29
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  • 74
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    Publication Date: 2011-08-16
    Description: An approximate analysis to estimate the quantity of nitric oxide that could be formed in the wake of a reentering lifting spacecraft is reported. Three different approaches are undertaken: two simplified analytical models utilizing the sudden-freezing concept named the 'trailing-edge-freezing' and 'wake-freezing' approximations, and a computer calculation involving numerical integration of chemical rate equations. The three methods predict a maximum nitric oxide production equivalent to 6, 9.5 and 8% of the mass of the spacecraft, respectively. Thus, the amount of nitric oxide expected to be produced by future space activities is negligibly small compared with that produced by the natural processes.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Atmospheric Environment; 10; 4, 19; 1976
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  • 75
    Publication Date: 2016-06-07
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Lunar Science Inst., Abstracts of Papers Presented at a Special Session of the Seventh Annual Lunar Science Conference on Utilization of Lunar Materials and Expertise for Large Scale Operations in Space; p 162-164
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  • 76
    Publication Date: 2016-06-07
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Lunar Science Inst., Abstracts of Papers Presented at a Special Session of the Seventh Annual Lunar Science Conference on Utilization of Lunar Materials and Expertise for Large Scale Operations in Space; p 158-159
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    Publication Date: 2016-11-16
    Description: A description of the orbiter science instruments is presented and the chronology of the two Viking missions is reviewed. The design of the Viking orbiter spacecraft is discussed, taking into account the propulsion subsystem, the attitude control subsystem, the planetary scan platform, aspects of command processing, problems of instrument operation and data processing, and data quantity limitations. Details concerning the Viking orbits and the visibility of the planet are also considered and the future of the Viking orbiter missions is evaluated. If the orbiters continue to perform well, all the orbiter science investigations will continue to acquire data for another year and perhaps somewhat longer.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Journal of Geophysical Research; Volume 82; Issue 28; 3971-3983
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  • 78
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    Publication Date: 2016-11-16
    Description: The Viking project launched two unmanned spacecraft to Mars in 1975 for scientific exploration with special emphasis on the search for life. Each spacecraft consisted of an orbiter and a lander. The landing sites were finally selected after the spacecraft were in orbit. Thirteen investigations were performed: three mapping experiments from the orbiter, one atmospheric investigation during the lander entry phase, eight experiments on the surface of the planet, and one using the spacecraft radio and radar systems. The experiments on the surface dealt principally with biology, chemistry, geology, and meteorology. Seventy-eight scientists have participated in the 13 teams performing these experiments. This paper is a summary of the project and an introduction to the articles that follow.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Journal of Geophysical Research; Volume 82; No. 28; 3959-3970
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  • 79
    Publication Date: 2011-08-17
    Description: Typical commercial or laboratory-prepared samples of polycrystalline AlSb contain microstructural inhomogeneities of Al- or Sb-rich phases in addition to the primary AlSb grains. The paper reports on gravitational influences, such as density-driven convection or sedimentation, that cause microscopic phase separation and nonequilibrium conditions to exist in earth-based melts of AlSb. A triple-cavity electric furnace is used to homogenize the multiphase AlSb samples in space and on earth. A comparative characterization of identically processed low- and one-gravity samples of commercial AlSb reveals major improvements in the homogeneity of the low-gravity homogenized material.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Metallurgical Transactions A - Physical Metallurgy and Materials Science; 10A; May 1979
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  • 80
    Publication Date: 2011-08-17
    Description: For Assess II, the Spacelab mission simulation conducted in mid-1977, four payload specialists aboard a Convair 990 research aircraft performed six American and six European experiments during nine research flights each of six hours duration in order to evaluate the compatibility of training and experimental design. Mission organization and some initial data from the European experiments are reported. The experiments, conducted over the western U.S., involved infrared astronomy, solar brightness temperature, lidar, airglow TV, and a medical experiment for which physiological parameters were monitored. Conclusions concerning general principles of experiment design are discussed.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Nature; 275; Sept. 7
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  • 81
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    Publication Date: 2011-08-17
    Description: Consideration is given to the potential role of robotics and automation in space transportation systems. Automation development requirements are defined for projects in space exploration, global services, space utilization, and space transport. In each category the potential automation of ground operations, on-board spacecraft operations, and in-space handling is noted. The major developments of space robot technology are noted for the 1967-1978 period. Economic aspects of ground-operation, ground command, and mission operations are noted.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 16; Sept
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  • 82
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    Publication Date: 2011-08-17
    Description: These series have included flyby, lunar-orbiting, and soft-landing missions. A variety of experiments were carried out by these spacecraft including studies of magnetism, X-ray and gamma ray emissions, gravitational anomalies, and chemical composition. Soil samples, near- and farside photography (both color and black and white), and earth-cloud photography were also acquired.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Catalog of Lunar Mission Data; p 153-164
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  • 83
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    Publication Date: 2011-08-17
    Description: Lunar spacecraft missions and the Ranger spacecraft are described. These spacecrafts were designed to achieve lunar impact trajectories and to transmit high resolution photographs of the lunar surface during the final minutes of flight. The television experiments are briefly evaluated.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Catalog of Lunar Mission Data; p 9-12
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  • 84
    Publication Date: 2011-08-17
    Description: Continuous and discontinuous lithium fluoride fibers embedded in a sodium chloride matrix were produced in space and on earth, respectively. The production of continuous fibers in an eutectic mixture was attributed to the absence of convection current in the liquid during solidification in space. Image transmission and optical transmittance measurements of transverse sections of the space-grown and earth-grown ingots were made with a light microscope and a spectrometer. It was found that better optical properties were obtained from samples grown in space. This was attributed to a better alignment of lithium fluoride fibers along the growth direction.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Apollo-soyuz Test Project; 27 p
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  • 85
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    Publication Date: 2011-08-17
    Description: The positive effects of microgravity on crystal quality and the fundamental properties of the vapor transport reaction were established by analyzing the results of three transport experiments on multicomponent systems performed during the Apollo-Soyuz Test Project mission. The systems employed were GeSe0.99Te0.01-GeI4(A), GeS0.98Se0.02-GeCl4(B), and GeS-GeCl4-Ar (C). The crystallographic analysis is based on a direct comparison of space and ground-based (prototype) crystals employing X-ray diffraction, microprobe, microscopic, and chemical etching techniques. The results demonstrate a considerable improvement of the space-grown crystals in terms of chemical and crystalline homogeneity, surface morphology, and bulk perfection relative to ground specimens.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Apollo-Soyuz Test Project; 40 p
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  • 86
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    Publication Date: 2011-08-17
    Description: The magnetic compounds under study, manganese-bismuth (MnBi) copper-cobalt-cerium (Cu,Co)5Ce, are representative of magnetic alloy systems that have the potential for the development of high coercive strength and a high energy product. The samples of 50 at. % bismuth and 50 at. % manganese solidified in the low-g environment demonstrated a substantial improvement in the macroscopic chemical homogeneity. The bismuth/manganese-bismuth directionally solidified eutectic flight samples exhibited marked superior magnetic properties. Intrinsic coercive strengths in excess of 185 Koe have been measured in the low-g processed samples at 77 K. The average value of inductance was improved by 76 percent, and the energy product was improved by 57 percent. Additional results indicate that, in the near-absence of the gravitational body force, contained fluids will assume a lowest energy configuration that differs significantly from that found terrestrially.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Apollo-Soyuz Test Project; 53 p
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  • 87
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    Publication Date: 2011-08-17
    Description: Goods and services that may be furnished by the Space Shuttle are described. A single multibeam antenna array capable of supplying satellite communication for 256 U.S. cities, a disaster warning network, and a TV link to remote areas is discussed. Attention is also given to such materials processing programs as crystal growth (for example, production of mercuric iodide crystals for gamma-ray detectors), eutectic growth of solid-solution crystals such as mercury-cadmium-telluride, manufacture of uniform latex spheres for medical applications, and development of small glass spheres for fusion power applications. In addition to the Space Telescope, a meter-class telescope on the Shuttle and a wide-field survey instrument are under study.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 16; Jan. 197
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  • 88
    Publication Date: 2011-08-17
    Description: The paper reviews the physical and chemical characteristics of lunar surface materials noting the thickness of the regolith, grain size distribution, regolith petrography, and the chemical composition of the regolith. A comprehensive design of a processing system for the production of structural metals, oxygen, silicon, glass, and ceramic materials is presented. Specifications regarding the location of the processing plant, and its mass, volume, and power requirements are reviewed.
    Keywords: ASTRONAUTICS (GENERAL)
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  • 89
    Publication Date: 2011-08-17
    Description: The paper examines some of the key technologies and forms of construction know-how that will have to be developed and tested for eventual application to building large structures in space. Construction of a shuttle-tended space construction/demonstration platform would comprehensively demonstrate large structure technology, develop construction capability, and furnish a construction platform for a variety of operational large structures. Completion of this platform would lead to demonstrations of the Satellite Power System (SPS) concept, including microwave transmission, fabrication of 20-m-deep beams, conductor installation, rotary joint installation, and solar blanket installation.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 15; Dec. 197
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  • 90
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    Publication Date: 2011-08-17
    Description: Some of the possible areas of application for large antennas placed in space are discussed, and some initial design concepts for various antenna proposals are described. Applications include rural mobile communications, an orbiting deep space relay station, submillimeter radio astronomy, and multispectral radiometry of earth surface features. As a first step in developing the needed technology, a deployable 30-m antenna with 1-mm surface accuracy is proposed. Flight experience with such an antenna system would enable validation of performance prediction models. The 30-m-diam mesh deployable-defurlable antenna experiment would be carried out with the shuttle.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 15; Dec. 197
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  • 91
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    Publication Date: 2011-08-16
    Description: The technical and nontechnical objectives of the Apollo-Soyuz mission are briefly considered. The mission demonstrated that Americans and Russians can work together to perform a very complex operation, including rendezvous in space, docking, and the conduction of joint experiments. Certain difficulties which had to be overcome were partly related to differences concerning the role of the astronaut in the basic alignment and docking procedures for space vehicles. Attention is also given to the experiments conducted during the mission and the approach used to overcome the language barrier.
    Keywords: ASTRONAUTICS (GENERAL)
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  • 92
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    Publication Date: 2011-08-16
    Description: A general overview is given of experiment planning and implementation for the ATS-6. Included in the review are discussions of project office activities, experiment selection, spacecraft implementation, ground terminal implementation, the operations control center, and the information processing division. A table is included summarizing the various experiments among which are communications, scientific and technological experiments.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: IEEE Transactions on Aerospace and Electronic Systems; AES-11; Nov. 197
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  • 93
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    Publication Date: 2011-08-16
    Description: It is pointed out that a space manufacturing facility may be economically more effective than alternative industries on the earth for the construction of products which are to be used in geosynchronous or higher orbits. The suggestion is made to construct solar power stations at a space colony and relocate them in geosynchronous orbit to supply energy to the earth. Attention is given to energy problems and approaches for solving them, taking into account environmental effects and economic factors. Economic aspects of space manufacturing are discussed in some detail.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Science; 190; Dec. 5
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  • 94
    Publication Date: 2011-08-17
    Description: The probability of satellite collisions increases with the number of satellites. In the present paper, possible time scales for the growth of a debris belt from collision fragments are determined, and possible consequences of continued unrestrained launch activities are examined. Use is made of techniques formerly developed for studying the evolution (growth) of the asteroid belt. A model describing the flux from the known earth-orbiting satellites is developed, and the results from this model are extrapolated in time to predict the collision frequency between satellites. Hypervelocity impact phenomena are then examined to predict the debris flux resulting from collisions. The results are applied to design requirements for three types of future space missions.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Journal of Geophysical Research; 83; June 1
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  • 95
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    Publication Date: 2011-08-17
    Description: The structure and origin of comets are reviewed with reference to future cometary research involving fly by and rendezvous missions. Ion-driven spacecraft, to be launched from a Shuttle in the mid-1980s, will theoretically be able to make close observations of Halley's Comet, and fly on to either Tempel 2 or Borelly's Comet during the course of the same mission. A rendezvous, whereby the spacecraft follows a comet in its path around the sun, is considered preferable to a fly by, which will allow only a few hours of observation. Suggested equipment for comet research include IR sensors, X- and Gamma-ray spectrometers, and possibly SEM to analyze the composition of cometary dust particles.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Technology Review; 80; Mar
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  • 96
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    Publication Date: 2011-08-17
    Description: Early U.S. space experiments involving the liquid propellant German V-2 are discussed. Although the primary objective of the experiments conducted under project Hermes after World War II was initially the development of missile technology, scientific objectives were soon given the priority. The missile was modified for scientific experiments and the payload increased from 6.8% to 47% between 1946 and 1949. Among other instruments, the payload included a cosmic ray telescope, ionosphere transmitter and spectrograph for solar spectral measurements. While the scientific success of the program established a positive public attitude towards space research, the Upper Atmosphere Research Panel, formed to coordinate the project, set a pattern for future scientific advisory bodies.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: vol. 32; Dec. 197
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  • 97
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    Publication Date: 2011-08-18
    Description: Progress in science in relation to the space shuttle is reported. Several studies on the uses of the space shuttle and Spacelab are highlighted. A review of the activities of the Shuttle Spacelab Payloads Project Office are presented. The activities cover such fields as solar physics, astronomy with optical instruments, high energy astrophysics, atmospheric research and magnetospheric physics, and Earth observational studies.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Proc. of the Shuttle-Based Cometary Sci. Workshop; p 193-197
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  • 98
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    Publication Date: 2011-08-18
    Description: Knowledge of chemical composition derived from the spectroscopy of small cometary meteoroids when they enter the Earth's atmosphere at high velocity and become visible as meteors is briefly summarized. For statistically reliable results it is necessary to have a large number of observations and this requires the photography of relatively faint meteors, which are considerably more numerous than the bright fireballs. The improvement in observational techniques and cameras has made it possible to extend the range of spectrographic data from cometary particles of mass between a kilogram and a gram down to those of only 0.01 or 0.001 grams in mass. The corresponding increase in the number-value of the statistics was from less than 100 data points to several 1000.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: NASA. Marshall Space Flight Center Proc. of the Shuttle-Based Cometary Sci. Workshop; p 150-159
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  • 99
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    Publication Date: 2011-08-17
    Description: The Cosmic Background Explorer satellite will measure the diffuse microwave and infrared emission from the universe over the entire wavelength range from a few microns to 13 mm with unprecedented sensitivity and accuracy. It will measure the spectrum and angular distribution of the cosmic background radiation thought to be remnant of the big bang explosion, and it may also detect the radiation produced by the primal stars and galaxies. Furthermore, it will gather a large body of data permitting detailed study of the distribution, spectra, and temperature of the interstellar and interplanetary dust.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Astronautics and Aeronautics; 16; Oct. 197
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  • 100
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    Publication Date: 2011-08-17
    Description: Vacuum conditions to be encountered in the wakes of high altitude unmanned space vehicles are calculated in order to demonstrate possibilities for conducting experiments using the high pumping speeds and very high vacuum (down to 10 to the -15th torr) attainable. The flux of ambient particles backscattered by emissions from spacecraft surfaces is modelled for an idealized Long Duration Exposure Facility spacecraft structure in an orbit of 550 km altitude. The total backscattered fluxes are found to be between 3 x 10 to the 4th and 3 x 10 to the 5th per sq cm sec for H and between 10 to the 6th and 10 to the 7th per sq cm sec for He and O, depending on the angle with respect to the wake axis. It is found that the direct ambient hydrogen flux is an order of magnitude greater than the backscattered flux, while the backscattered fluxes of He and O are greater than the direct fluxes. It is pointed out that care should be taken in designing space experiments to enable these theoretical conditions to be met.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: Vacuum; 28; Feb. 197
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