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  • 1
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    Indicial Aerodynamics (1961)
    In:  CASI
    Details
    Publikationsdatum: 2011-12-14
    Beschreibung: Indicial aerodynamics
    Schlagwort(e): BIOTECHNOLOGY
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  • 2
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    Buffeting tests in a cryogenic windtunnel (1995)
    In:  Other Sources
    Details
    Publikationsdatum: 2011-08-24
    Beschreibung: Measurements of wing buffeting, using root strain gages, were made in the NASA Langley 0.3 m cryogenic wind tunnel to refine techniques which will be used in larger cryogenic facilities such as the United States National Transonic Facility (NTF) and the European Transonic Wind Tunnel (ETW). The questions addressed included the relative importance variations in frequency parameter and Reynolds number, the choice of model material (considering both stiffness and damping) and the effects of static aeroelastic distortion. The main series of tests was made on three half models of slender 65 deg delta wings with a sharp leading edge. The three delta wings had the same planform but widely differing bending stiffnesses and frequencies (obtained by varying both the material and the thickness of the wings). It was known that the steady flow on this configuration would be insensitive to variations in Reynolds number. On this wing at vortex breakdown the spectrum of the unsteady excitation is unusual, having a sharp peak at particular frequency parameter. Additional tests were made on one unswept half-wing of aspect ratio 1.5 with an NPL 9510 aerofoil section, known to be sensitive to variations in Reynolds number at transonic speeds. The test Mach numbers were M = 0.21 and 0.35 for the delta wings and to M = 0.30 for the unswept wing. On this wing the unsteady excitation spectrum is fairly flat (as on most wings). Hence correct representation of the frequency parameter is not particularly important.
    Schlagwort(e): AERODYNAMICS
    Materialart: Aeronautical Journal (ISSN 0001-9240); 99; 981; p. 1-14
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  • 3
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    The Apollo food program (1970)
    In:  Other Sources
    Details
    Publikationsdatum: 2011-12-21
    Beschreibung: Modifications for Apollo space flight feeding program
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: AEROSPACE FOOD TECHNOL. 1970; P 5-13
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  • 4
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    Impact (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Impact, emergency escape and crash survival protection are studied. Accleration, the G system of units, data interpretation, and human tolerance limits are summarized, along with physiological and biochemical response to impact. Biomechanical factors of impact are also cited.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 221-295
    Format: text
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  • 5
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    Ablator manufacturing (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Studies are being conducted to determine how manufacturing-induced defects affect the performance of ablative heat shields. If commonly occurring defects do not affect material performance, simpler manufacturing techniques can be used, quality control requirements can be relaxed, repair and rework operations can be held to a minimum, and thus the total manufacturing cost can be reduced.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA Space Shuttle Technol. Conf.; p 475-504
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  • 6
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    Manufacturing developments in insulation application (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Manufacturing development studies have been conducted to provide information on the fabrication and handling characteristics of a number of candidate multilayer insulation systems. The application of these complex, lightweight insulation systems to large-scale, flight-type cryogenic tankage and other structures has of necessity required the development of new methods, processes, and tooling concepts. Results of some of the studies that have contributed to the advancement of cryogenic technology are presented. The insulation systems that are of primary importance for future application are those using the sliced foam spacers, the net type spacers, the glass fiber paper spacers, and the Superfloc system which consists of tufts of dacron fibers flocked on the surface of the radiation shields.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Cryog. Res. at MSFC: Res. Achievements Rev., Vol. 4, No. 2; p 73-92
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  • 7
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    Design for advanced insulation systems (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The design of principal multilayer insulation (MLI) systems being investigated by Marshall Space Flight Center and its contractors for application to flight-type cryogenic tankage for long-term storage in space vehicles is described. The MLI systems were designed for application to a 105 in. diameter cryogenic test tank to simulate full-scale design and installation methods representative of flight-type hardware. The MLI systems selected for design represent systems suitable for use on space vehicles such as the modular nuclear vehicles that require application of thicknesses up to 6 in. The MLI systems are lightweight and structurally efficient.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Cryog. Res. at MSFC: Res. Achievements Rev., Vol. 4, No. 2; p 53-72
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  • 8
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    Multilayer high performance insulation materials (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: A number of tests are required to evaluate both multilayer high performance insulation samples and the materials that comprise them. Some of the techniques and tests being employed for these evaluations and some of the results obtained from thermal conductivity tests, outgassing studies, effect of pressure on layer density tests, hypervelocity impact tests, and a multilayer high performance insulation ambient storage program at the Kennedy Space Center are presented.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Cryog. Res. At MSFC: Res. Achievements Rev., Vol. 4, No. 2; p 93-98
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  • 9
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    Fire extinguishment in hypobaric and hyperbaric environments (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Work that has been performed to provide information on the effects of various fire extinguishing agents in special atmospheres is discussed. Data used in the development of both equipment and techniques for manned spacecraft and related equipment are discussed. The equipment includes a hypobaric chamber suitable for low pressure use and a hyperbaric chamber for high pressure operation. The effectiveness of agents in weightless environment is also discussed.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Conf. on Mater. for Improved Fire Safety; p 163-169
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  • 10
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    Specialized testing and evaluation of space-suit materials (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The selection of nonmetallic materials used in the Apollo space suits is discussed. The specialized test program to determine the flammability of selected space suit materials is described. Emphasis is placed on the equipment used to test and qualify the space suit materials and subassemblies for operation in the deep space environment.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: Conf. on Mater. for Improved Fire Safety; p 187-190
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  • 11
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    The combustion process (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The effect of thermodynamic, chemical, and physical properties on the combustion of materials is discussed. The mechanisms which produce and support combustion of various materials are examined. The effects of free radical reactions, convection and gravitational effects on combustion rates, and changes in flame propagation due to size and shape of surfaces are described.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Conf. on Mater. for Improved Fire Safety; p 3-7
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  • 12
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    Feeding man in space (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Semi-solid, dehydrated, rehydratable, thermally stabilized wet, and intermediate moisture food development for space flights
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON PROC. OF THE 7TH ANN. WORKING GROUP ON EXTRATERREST. RESOURCES 1970; P 39-49
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  • 13
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    Conditions for local thermodynamic equilibrium in uranium (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Model for calculation of parameters for local thermodynamic equilibrium in uranium
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: FLORIDA UNIV. RES. ON URANIUM PLASMAS AND THEIR TECHNOL. APPL. 1971; P 173-178
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  • 14
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    Application of advanced aerodynamics to future transport aircraft (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Applications of supercritical airfoils to transport aircraft designs
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA AIRCRAFT SAFETY AND OPERATING PROBL., VOL. 1 1971; P 165-176
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  • 15
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    Aircraft response to the wing trailing vortices generated by large jet transports (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Flight tests for evaluating effect of wing-tip vortex wake generated by large jet transports on smaller aircraft
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA AIRCRAFT SAFETY AND OPERATING PROBL., VOL. 1 1971; P 115-126
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  • 16
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    Progress report on wing-trailing-vortex studies (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Effect of wing-tip vortex wakes generated by large jet transport aircraft on smaller airplanes
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA AIRCRAFT SAFETY AND OPERATING PROBL., VOL. 1 1971; P 101-113
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  • 17
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    Gust alleviation (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Alleviation of lateral and longitudinal gust effects on aircraft
    Schlagwort(e): AERODYNAMICS
    Materialart: PERFORMANCE AND DYN. OF AEROSPACE VEHICLES 1971; P 505-553
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  • 18
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    Human response in closed loop control of dynamic systems (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Linear transfer function for describing human response to aircraft control
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: PERFORMANCE AND DYN. OF AEROSPACE VEHICLES 1971; P 555-577
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  • 19
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    Effects of aeroelasticity on static aerodynamic derivatives (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Effects of aeroelasticity on static longitudinal aerodynamic derivatives
    Schlagwort(e): AERODYNAMICS
    Materialart: PERFORMANCE AND DYN. OF AEROSPACE VEHICLES 1971; P 375-438
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  • 20
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    Design of bodies for low drag and high performance in practical hypersonic flight (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Minimizing drag and increasing performance of optimum shapes at hypersonic flight
    Schlagwort(e): AERODYNAMICS
    Materialart: PERFORMANCE AND DYN. OF AEROSPACE VEHICLES 1971; P 103-174
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  • 21
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    Methods of obtaining stability derivatives (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Least squares method and iteration technique for obtaining aerodynamic stability derivatives
    Schlagwort(e): AERODYNAMICS
    Materialart: PERFORMANCE AND DYN. OF AEROSPACE VEHICLES 1971; P 71-101
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  • 22
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    Thermal design of a satellite telescope (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Thermal control techniques in designing large orbiting telescopes
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA, WASHINGTON OPT. TELESCOPE TECHNOL. 1970; P 359-379
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  • 23
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    Food development and experiences (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Compressed dehydrated food for aircraft crews
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 117-119
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  • 24
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    Design considerations for microwave heating of space food (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Reliability, weight, size, and power supplies as factors in designing microwave ovens for spacecraft
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 175-176
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  • 25
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    Airborne microwave oven development (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Research and development of microwave ovens for use in aircraft
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 171-174
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  • 26
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    Integral heating equipment development (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Laboratory and flight performance tests of integral heating units for food preparation
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 177-181
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  • 27
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    Thermodynamics of the internal combustion engine (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Pollution aspects of internal combustion engine thermodynamics
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: ET. AND THERMODYN. IN HIGH TEMP. GASES 1970; P 31-40
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  • 28
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    Pacing technology (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Projected research and development for selected and alternative subsystems of integrated life support system
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 697-713
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  • 29
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    CO2 removal and concentration (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Steam desorbed resin for carbon dioxide removal in spacecraft cabin atmosphere
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 157-205
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  • 30
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    Analysis of the flow field of a jet in a subsonic crosswind (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Jet induced flow field effects on V/STOL aircraft in subsonic transition flight
    Schlagwort(e): AERODYNAMICS
    Materialart: L. METHODS IN AIRCRAFT AERODYN. 1970; P 683-702
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  • 31
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    Procedures for designing supersonic bodies of revolution from prescribed surface pressure distributions (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Iterative method for designing supersonic body of revolution from surface pressure distribution
    Schlagwort(e): AERODYNAMICS
    Materialart: L. METHODS IN AIRCRAFT AERODYN. 1970; P 75-84
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  • 32
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    Work, heat, and oxygen cost (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Human energy is discussed in terms of the whole man. The physical work a man does, the heat he produces, and the quantity of oxygen he takes from the air to combine with food, the fuel source of his energy, are described. The daily energy exchange, work and heat dissipation, oxygen costs of specific activities, anaerobic work, and working in space suits are summarized.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 847-879
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  • 33
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    Human control capabilities (1973)
    In:  CASI
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    Publikationsdatum: 2005-11-30
    Beschreibung: The capabilities and limitations of man as an element in a closed loop control system under normal environmental conditions are described. Controller characteristics are enumerated, using manual control, quasilinear models, pilot opinion and ratings, compensatory tracking, optimum control models, motion cues, multiple input tracking, multiple loop tracking, transmission delays, and adaptive manual control. Various controls, manipulators, and displays are also considered.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 751-806
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  • 34
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    Noise and blast (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Noise and blast environments are described, providing a definition of units and techniques of noise measurement and giving representative booster-launch and spacecraft noise data. The effects of noise on hearing sensitivity and performance are reviewed, and community response to noise exposure is discussed. Physiological, or nonauditory, effects of noise exposure are also treated, as are design criteria and methods for minimizing the noise effects of hearing sensitivity and communications. The low level sound detection and speech reception are included, along with subjective and behavioral responses to noise.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 693-750
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  • 35
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    Rotary acceleration (1973)
    In:  CASI
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    Publikationsdatum: 2005-11-30
    Beschreibung: Rotary acceleration is found to be a manifestation of angular acceleration, and is always present during steady state spinning or tumbling, even when the angular velocity is constant. Subjective reactions and tolerances, performance, physiological effects, and pathological effects are reviewed for rotary acceleration. Thresholds for stimulation perception by angular acceleration in man are presented in tabular form.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 191-219
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  • 36
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    Atmosphere (1973)
    In:  CASI
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    Publikationsdatum: 2005-11-30
    Beschreibung: Properties of elements and compounds are considered which make up or may be added to a gaseous environment suitable for humans. Oxygen and carbon dioxide are emphasized; nitrogen and the noble gases are also cited. Other gaseous compounds, such as carbon monoxide, methane, and sulfur hexafluoride, are briefly mentioned.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 35-63
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  • 37
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    Sustained linear acceleration (1973)
    In:  CASI
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    Publikationsdatum: 2005-11-30
    Beschreibung: The subjective effects of sustained acceleration are discussed, including positive, negative, forward, backward, and lateral acceleration effects. Physiological effects, such as retinal and visual response, unconsciousness and cerebral function, pulmonary response, and renal output, are studied. Human tolerance and performance under sustained acceleration are ascertained.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 149-190
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  • 38
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    Rocket combustion instability suppression with cavity resonators (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Properly tuned Helmholtz resonator damping devices are an effective method for eliminating high frequency combustion instability in rocket engine thrust chambers. A program was implemented with the objective of extending Helmholtz resonator theory to thrust chamber conditions to establish a standard design procedure. By using systematic cold-flow testing and hot firings, empirical design equations were formulated. An effort is currently underway to extend the design theory to other types of acoustical damping devices such as quarter-wave tubes and slots.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Res. Achievements Rev., Vol. 4, No. 6; p 53-59
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  • 39
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    Combined environmental stresses (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Tolerance levels, physiological effects, and performance degradation during simultaneous or sequential exposures to two environmental stresses, and also three or more simultaneous stresses are described. Environmental stress combinations are characterized by four descriptors: order of occurrence, duration of exposure, severity of exposure, and type of interaction. Combined stress data and facilities for combined stress study are briefly mentioned.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 881-914
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  • 40
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    Temperature (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The problems in human comfort in heat stress are emphasized, with less emphasis placed upon cold exposure problems. Physiological parameters related to human thermal interactions are discussed, as well as data concerning thermal protective clothing. The energy balance equation, heat transfer equation, thermal comfort, heat stress, and cold stress are also considered. A two node model of human temperature regulation in FORTRAN is appended.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 65-148
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  • 41
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    Reusable surface insulation materials research and development (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Reusable surface insulation is considered a prime candidate for heat shielding large areas of the space shuttle vehicle. The composition and fabrication of RSI materials are discussed, followed by evolution of RSI and current problems, physical and thermal properties, arc plasma test data and results, and material improvement research. Finally, a summary of RSI technology status is presented.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA Space Shuttle Technol. Conf.; p 373-433
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  • 42
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    Materials and design for ablative heat shields (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The goal of the ablation technology program is to bring ablation research and development to a high state of readiness for application to space shuttle vehicles. Some recent results and current work in the areas of materials, designs, and refurbishment for ablative TPS are reported. Future research and development needs are also presented.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA Space Shuttle Technol. Conf.; p 505-536
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  • 43
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    Thermal protection system trade studies on ablators and reuseable surface insulation (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Analytical trade studies are presented that consider passive TPS configurations using the following material categories: (1) reuseable surface insulation - surface-coated rigidized ceramic fiber; (2) low density charring ablators; and (3) carbon-carbon and high density ablators for leading edge areas. Emphasized are effects on TPS weight by variations in entry trajectories and material thermal characteristics.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA Space Shuttle Technol. Conf.; p 303-334
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  • 44
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    An assessment of radiative metallic thermal protection systems for space shuttle (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The metallic thermal protection system technology program for the space shuttle is reviewed for the areas of environmental uncertainties, materials data base, TPS design concepts and heat-shield panel configurations, testing and evaluation of materials, panels, and complete systems.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA Space Shuttle Technol. Conf.; p 267-302
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  • 45
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    Development of a silicone ablator for high-heat-flux and high-shear-rate condition (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: A silicone material was developed which gives suitable ablative protection in the high heat flux, high shear environments encountered in severe reentry applications, such as nose cones for ballistic vehicles and protection of leading edges or other critical areas of a vehicle. In addition, the ease of handling, low application cost, and room temperature cure make such a silicon material suitable nozzles for the large rockets necessary for vehicle launching. The development of this product is traced from the selection of suitable polymers through the choice of fillers and the finalization of filler loadings.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA. Goddard Space Flight Center Space Simulation; p 725-748
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  • 46
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    Space simulation and rate dependent radiation testing (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: An environmental test facility is described which allows in-situ measurements for evaluation of near real time sinergistic effects of combined space environments.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA. Goddard Space Flight Center Space Simulation; p 453-460
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  • 47
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    Multilayer insulation thermal protection systems technology (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: A summary is presented of the work performed by Marshall Space Flight Center (MSFC) and industry toward the development of flight-type multilayer insulation(MLI) systems. The MSFC MLI program is divided into three large categories: (1) the generation and compilation of MLI composite test data; (2) the analysis, design, and testing of heat flow through MLI applied to ducting, seams, electrical feedthroughs, structural supports, and the tank sidewall; and (3) the development, modification, and utilization of new testing procedures, tanks, and the test facilities. Numerous data have been generated, analyzed, and documented on different MLI composites.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Cryog. Res. at MSFC: Achievements Rev., Vol.4, No. 2; p 5-52
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  • 48
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    Nozzle exhaust plume backscatter experiment using the JPL Molsink facility (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Qualitative tests were made by injecting water through a rocket nozzle wall, and the droplet trajectories were observed photographically. These tests were conducted for nozzles in which boundary layer flow is significant. The tests indicated that both gases and particulate matter will be found in the region outside of the plume boundaries, and can be calculated using current analytical techniques. A test program is being conducted to measure the distribution of exhaust gases from small nozzles using an electron beam/photomultiplier system and a matrix of quartz crystal microbalances. Calibration tests, using simulated hydrazine exhaust product gas mixtures, were also conducted. The test program and results of the pumping calibration tests with hydrazine (simulated hydrazine exhaust products) are reported.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: JPL Quart. Tech. Rev., Vol. 1, No. 4; p 89-96
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  • 49
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    Considerations on precision temperature control of a large orbiting telescope (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Precision temperature control of large orbiting telescopes
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: OPT. TELESCOPE TECHNOL. 1970; P 417-424
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  • 50
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    General Foods Corporation product development as related to aerospace food problems (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Shelf-stable rehydratable and intermediate moisture foods and moisture mimetic products
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 125-129
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  • 51
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    Quantifying and improving Manned Orbiting Laboratory food (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Human factors and standardization of food item selection for Manned Orbiting Laboratory feeding system
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 21-29
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  • 52
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    Food synthesis by physicochemical methods (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Physicochemical synthesis of food for long term space flights
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: AEROSPACE FOOD TECHNOL. 1970; P 133-140
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  • 53
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    Pan American World Airways - Present and future plans (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Logistics of feeding Boeing 707 and 747 aircraft passengers
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 109-111
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  • 54
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    Airline versus space feeding (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Airline and space feeding systems, and work-rest division of astronauts day
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 105-108
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  • 55
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    Rate constants from ignition studies of the H2-CO-O2 system (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Rate constant determination for ignition of hydrogen carbon monoxide oxygen system
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: ET. AND THERMODYN. IN HIGH TEMP. GASES 1970; P 105-117
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  • 56
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    Ground-wind-load considerations for space shuttle vehicles (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Ground wind loads on reusable space shuttles
    Schlagwort(e): AERODYNAMICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 143-160
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  • 57
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    Buffet and aerodynamic noise (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Space shuttle buffeting and aerodynamic noise
    Schlagwort(e): AERODYNAMICS
    Materialart: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 238-247
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  • 58
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    Theoretical investigation of ducted fan interference for transport-type aircraft (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Ducted fan interference analysis for transport aircraft
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 703-719
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  • 59
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    Time-dependent numerical method for treating complicated blunt-body flow fields (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Time-dependent numerical method for blunt body flow field solutions
    Schlagwort(e): AERODYNAMICS
    Materialart: L. METHODS IN AIRCRAFT AERODYN. 1970; P 177-195
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  • 60
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    A critical evaluation of analytic methods for predicting laminar-boundary-layer shock-wave interaction (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Prediction methods for boundary layer and flow field characteristics in shock wave-boundary layer interaction
    Schlagwort(e): AERODYNAMICS
    Materialart: L. METHODS IN AIRCRAFT AERODYN. 1970; P 515-539
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  • 61
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    A numerical method for computing three-dimensional viscous supersonic flow fields about slender bodies (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Numerical analysis of three dimensional viscous supersonic flow fields about slender bodies
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA, WASHINTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 265-321
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  • 62
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    In-flight aeroacoustic environments on prospective space shuttle vehicles (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The problem of in-flight aerodynamic noise has been studied by reliable estimates of full scale surface-pressure fluctuations from scale model tests in wind tunnels. Scaling relationships have been verified, and many details of the fluctuating pressure characteristics such as spatial correlation and convection velocities are understood. The effects of the wind tunnel environmental turbulence and noise have also been investigated sufficiently so that threshold levels of usable data are known.
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA Space Shuttle Technol. Conf.; p 71-96
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  • 63
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    Oxidation protected carbon-carbon (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Pyrolized carbon-carbon has one unique advantage over other materials that makes its application to the space shuttle thermal protection system very attractive. This unique characteristic is the increase in material strength and modulus with increase in temperature up to about 2500 K (4040 F). Offsetting this unique advantage are disadvantages which include brittleness, high cost, and the tendency of the material to react with oxygen, particularly at high temperatures. The development of an oxidation inhibitor for the material and the definition of fabrication processes for selected full-scale components are considered.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA Space Shuttle Technol. Conf.; p 335-372
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  • 64
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    Development of materials screening tests for oxygen-enriched environments (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The criteria governing materials to be used in an oxygen enriched atmosphere and tests to determine suitability for fireproof considerations in spacecraft design are discussed. The nine tests applied to materials before acceptance in spacecraft construction are presented. The application of the standard tests to determine ranking of materials is included.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Conf. on Mater. for Improved Fire Safety; p 23-27
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  • 65
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    Long-term space mission requirements (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Possible feeding systems for long term space missions after Apollo Applications Program
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 145-149
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  • 66
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    Food system integration responsibilities of airframe manufacturers (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Food system integration into aircraft as joint responsibility of airframe manufacturers and air carriers
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 193-202
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  • 67
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    Boeing 747 lower lobe galley system integration (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: System integration of Boeing 747 lower lobe galley
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 183-191
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  • 68
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    Werner Sell equipment development (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: High temperature oven with fast-circulated hot air as possible equipment for spacecraft
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 169-170
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  • 69
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    Japan Air Lines - Present and future plans (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Transworld airline feeding operations
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 112-114
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  • 70
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    Systems analysis of Manned Orbiting Laboratory feeding system (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Systems analysis of feeding system for Manned Orbiting Laboratory
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 43-55
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  • 71
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    Atmospheric contamination control (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Trace gas control method for decontamination of integrated life support system
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 253-283
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  • 72
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    Optimization of supersonic inlets using the method of characteristics (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Method of characteristics for computerized design of optimal supersonic inlets
    Schlagwort(e): AERODYNAMICS
    Materialart: L. METHODS IN AIRCRAFT AERODYN. 1970; P 569-581
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  • 73
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    A new method for calculating near and far field pressure about arbitrary configurations (1970)
    In:  CASI
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    Publikationsdatum: 2005-11-27
    Beschreibung: Aerodynamic method of characteristics for pressure field calculations about wing-body combinations
    Schlagwort(e): AERODYNAMICS
    Materialart: L METHODS IN AIRCRAFT AERODYN. 1970; P 215-227
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  • 74
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    The analysis of propeller-wing flow interaction (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Numerical analysis of propeller-wing flow interaction with slipstreams
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 721-742
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  • 75
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    Diluent study (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Weight and power aspects of integrated life support system having either nitrogen, helium, or neon atmosphere
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 715-738
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  • 76
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    Selected EC/LS systems (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Environmental control and life support systems design criteria for prolonged manned space flight mission
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 573-696
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  • 77
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    Waste control (1970)
    In:  CASI
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    Publikationsdatum: 2005-11-27
    Beschreibung: Vacuum decomposition of human waste materials during prolonged space flight in controlled atmosphere
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 425-472
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  • 78
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    Oxygen and nitrogen storage (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Oxygen and nitrogen storage requirements for integrated life support system
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 65-108
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  • 79
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    Conduct of study (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Outline of study on regenerative advanced integrated life support systems
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 9-64
    Format: text
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  • 80
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    Water electrolysis (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Water electrolysis system for carbon dioxide reduction and oxygen generation in closed cabin atmosphere
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 117-156
    Format: text
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  • 81
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    Ionizing radiation (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The penetrating ionizing space radiations are found to be extremely diverse in the energy range of both their particulate and their electromagnetic components. Radiation terms and measures and ionizing radiation classes and sources are presented. Whole body radiation effects are examined, including radiation intensity and rate effectiveness factors. Radiation effects on specific body systems, such as blood, skin, visual, and reproductive systems are also discussed.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 417-454
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 82
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    Barometric pressure (1973)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The effects of alterations in barometric pressure on human beings are described. Human tolerances for gaseous environments and low and high barometric pressure are discussed, including effects on specific areas, such as the ear, lungs, teeth, and sinuses. Problems due to trapped gas within the body, high dynamic pressures on the body, and blasts are also considered.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 1-34
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 83
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    Heat pipes for spacecraft temperature control: Their usefulness and limitations (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Heat pipes are used in spacecraft to equalize the temperature of structures and maintain temperature control of electronic components. Information is provided for a designer on: (1) a typical mounting technique, (2) choices available in wick geometries and fluids, (3) tests involved in flight-qualifying the design, and (4) heat pipe limitations. An evaluation of several heat pipe designs showed that the behavior of heat pipes at room temperature does not necessarily correlate with the classic equations used to predict their performance. They are sensitive to such parameters as temperature, fluid inventory, orientation, and noncondensable gases.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: 6th Aerospace Mech. Symp.; p 33-41
    Format: text
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  • 84
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    Materials for foam type insulation (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: An internal foam fabrication is one of the concepts being considered for cryogenic insulation on the hydrogen tanks of the shuttle vehicle. The three-dimensional polyurethane used on the S-4 B tanks failed to meet the higher temperature requirements of the shuttle vehicle, however, and other foams under consideration include polyisocyanurates, polyphenylene oxides, polyimides, and polybenzimidazoles. Improved adhesive systems for attaching the foams to the interior tank wall are under study.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Cryog. Res. at MSFC: Res. Achievements Rev., Vol. 4, No. 2; p 179-184
    Format: text
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  • 85
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    A review of the Grumman orbiter wind tunnel heat transfer tests (1972)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: Tests were conducted in the NASA Langley continuous flow, variable density and Mach 20 helium tunnels. The orbiter was tested alone and with various side and tandem mounted tanks. Test conditions spanned a Reynolds number range which resulted in both laminar and turbulent flows. Experimental studies also examined the heat transfer problems associated with integration of the auxiliary propulsion system into the orbiter. Tests in the hypersonic shock tunnel investigated heating to cavities and heating from single and multiple hydrogen-oxygen plumes while tests, run as part of the configuration evaluation, examined the heating to wing pods.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: NASA. Langley Res. Center Space Shuttle Aerothermodyn. Technol. Conf., vol. 2; p 297-345
    Format: text
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  • 86
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    Flammability tests for Apollo command module and lunar module mockup (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The flammability test program for Apollo command module and lunar module mockups is described. The fire safety design of the modules was verified by performing deliberate ignitions at many locations while the interior atmosphere was controlled to simulate realistic flight conditions. The data obtained for each test and restrictions on various materials are discussed.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Conf. on Mater. for Improved Fire Safety; p 43-54
    Format: text
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  • 87
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    Apollo space-suit materials (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The design, construction, and materials used in the Apollo space suit are discussed. The various materials and combinations of materials to obtain the desired type of protection are identified. Detailed descriptions are provided of the pressure garment, liquid cooled garment, extravehicular gloves, helmet, and boots.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: Conf. on Mater. for Improved Fire Safety; p 145-149
    Format: text
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  • 88
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    Manned spacecraft nonmetallic-materials flammability selection criteria and requirements (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: The criteria and requirements governing the selection and use of nonmetallic materials in manned spacecraft to control potential fire hazards are reviewed. The development of flammability requirements is discussed and traced through the historical evolution. Events that dictated the changes that have taken place are discussed. The current nonmetallic material requirements are presented. Significant features of a nonmetallic materials handbook are included.
    Schlagwort(e): THERMODYNAMICS AND COMBUSTION
    Materialart: Conf. on Mater. for Improved Fire Safety; p 9-21
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 89
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    Odor test (1971)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-30
    Beschreibung: To prevent the use of spacecraft material that would outgas objectionable or nauseating odors, an odor test was developed. This test provided a means whereby candidate spacecraft materials were subjected to a particular environment and the outgassed products were evaluated by an odor panel. This panel was comprised of individuals with acute olfactory senses. The test results of the odor panel provided design engineers with data regarding potential material-odor problems. The odor-test procedure, panel-member selection, and odor scoring methods are described and typical test results are presented.
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: Conf. on Mater. for Improved Fire Safety; p 203-205
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 90
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    Wind tunnel simulation of ground wind shear and turbulence spectra with possible application to space shuttle launch problems (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Wind tunnel simulation of ground wind shear and turbulence spectra and application to space shuttle launching
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 161-175
    Format: text
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  • 91
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    US Army food research and development program (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Different techniques of preserving food for military field rations
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 151-163
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 92
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    Biological foods (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Crude biomasses for nutritional requirements of spacecraft crews
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 141-144
    Format: text
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  • 93
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    Meat-type food development and experiences (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Dehydrated and rehydratable meat-type foods for space flight feeding
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 121-123
    Format: text
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  • 94
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    Food plans for Sealab 3 (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Food selection and preparation plans for Sealab 3
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 79-85
    Format: text
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  • 95
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    Apollo applications program requirements (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Requirements for Apollo Applications Program feeding system
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: AEROSPACE FOOD TECHNOL. 1970; P 57-60
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 96
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    Advantages, problems, and experiences of irradiated foods (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Advantages and problems of preserving food with ionizing radiation
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 87-100
    Format: text
    Standort Signatur Erwartet Verfügbarkeit
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  • 97
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    Evaluation of space feeding systems (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Functional analysis on feeding system for Manned Orbiting Laboratory
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 31-36
    Format: text
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  • 98
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    Development of new concepts for the feeding system for the USAF Manned Orbiting Laboratory (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Improved prototype space feeding system for Manned Orbiting Laboratory missions
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 37-41
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  • 99
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    Manned Orbiting Laboratory feeding system requirements (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Feeding system requirements for Manned Orbiting Laboratory
    Schlagwort(e): BIOTECHNOLOGY
    Materialart: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 15-19
    Format: text
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  • 100
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    Theoretical studies of vortex flow on slender wing-body combinations (1970)
    In:  CASI
    Details
    Publikationsdatum: 2005-11-27
    Beschreibung: Lift and pressure distribution calculations for winged body with leading edge vortices
    Schlagwort(e): AERODYNAMICS
    Materialart: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 113-129
    Format: text
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