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  • 42.75
  • Aircraft Propulsion and Power
  • Lunar and Planetary Science and Exploration
  • 2000-2004
  • 1970-1974  (10)
  • 1950-1954
  • 1970  (10)
Collection
Years
  • 2000-2004
  • 1970-1974  (10)
  • 1950-1954
Year
  • 1
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    Unknown
    In:  CASI
    Publication Date: 2015-02-11
    Description: Hybrid waveguide /H-guide/ with laminated dielectric slab
    Keywords: Aircraft Propulsion and Power
    Type: STUDY OF RECTANGULAR-GUIDE-LIKE STRUCT. FOR MILLIMETER WAVE TRANSMISSION 15 JUN. 1970; P 6-12
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  • 2
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    In:  CASI
    Publication Date: 2019-05-16
    Description: The Apollo 12 mission was the twelfth in a series of flights using Apollo flight hardware and was the second lunar landing. The purpose of the mission was to perform a precise lunar landing and to conduct a specific scientific exploration of a designated landing site in the Ocean of Storms. Since the performance of the entire spacecraft was excellent, this report discusses only the systems performance that significantly differed from that of previous missions. Because they were unique to Apollo 12, the lunar surface experiments, the precision landing operation, and lunar dust contamination are reported in sections 3, 4, and 6, respectively. A complete analysis of all flight data is not possible within the time allowed for preparation of this report. Therefore, report supplements will be published for certain Apollo 12 systems analyses, as shown in appendix E. This appendix also lists the current status of all Apollo mission supplements, either published or in preparation. Other supplements will be published as the need is identified. In this report, all actual times prior to earth landing are elapsed time from range zero, established as the integral second before lift-off. Range zero for this mission was 16:22:00 G.m.t., November 14, 1969. Greenwich mean time is used for all times after earth landing as well as for the discussions of the experiments left on the lunar surface. All references to mileage distance are in nautical miles.
    Keywords: Lunar and Planetary Science and Exploration
    Type: NASA-TM-X-74200 , MSC-01855
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  • 3
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    In:  Other Sources
    Publication Date: 2018-06-05
    Description: This episode (4th and last in the series) opens with Michael Collins in the Command Module, Columbia. It then shows the flight of the Lunar Excursion Module (LEM) and the rendezvous with Columbia. The reentry into the Earth's atmosphere, the parachutes deployment, followed by the splashdown is shown. Next we see shots of various parades welcoming the three astronauts home. Following these celebrations, we see the Lunar Receiving Lab, where the Lunar rocks are processed, and the various questions that science hopes to begin to answer about the moon, the development of the solar system and the evolution of life on earth, with the close examination of the rocks are asked.
    Keywords: Lunar and Planetary Science and Exploration
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  • 4
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    In:  Other Sources
    Publication Date: 2018-06-05
    Description: This episode (third in a four-part series), opens with various shots of the natural environment of the earth, after which we hear communications with the astronauts on board the Apollo 11 spacecraft, including the news of the day. Views of the approach to the moon, the descent to the lunar surface, and the landing, including the statement, "Houston, Tranquility Base here. The Eagle has Landed." are included. This is followed by the descent down the ladder to the surface of the moon by Neil Armstrong and the now famous words, "That's one small step for man, one giant leap for mankind." Various shots of crowds watching around the world are shown, followed by the descent down the ladder by Buzz Aldrin, and the planting of the American Flag. There are views of the astronauts moving around the lunar surface which are followed by a series of still shots of this historic occasion.
    Keywords: Lunar and Planetary Science and Exploration
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  • 5
    Publication Date: 2019-06-27
    Description: Airbreathing hypersonic aircraft employing liquid hydrogen fuel have the potential of satisfying a number of mission requirements in the 1980-2000 time period. However, major advances in the technological state of the art are necessary before such aircraft can be considered either feasible or practical. The objective was to assess the research and development requirements for hypersonic aircraft and based on these requirements, to provide the NASA with characteristics of a number of desirable hypersonic research facilities. The study is organized in three phases. Phase I was a preliminary analysis of a broad group of concepts which were reduced to seven flight research facilities and eleven ground research facilities for Phase II study. The purpose of Phase II was to perform parametric studies to refine the facility designs and obtain sensitivity information in the neighborhood of "near optimum" designs, and to select those facilities that appear most attractive in the sense of research potential vs cost for further refinement in Phase III. This part of Volume III presents the results of the synthesis of the flight research facilities.
    Keywords: Aircraft Propulsion and Power
    Type: NASA-CR-114326 , MDC-A0013-VOL-3-PT-2
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  • 6
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    In:  CASI
    Publication Date: 2019-08-28
    Description: Apollo 13, the third U.S. manned lunar landing mission, will be launched April 11 from Kennedy Space Center, Fla., to explore a hilly upland region of the Moon and bring back rocks perhaps five billion years old. The Apollo 13 lunar module will stay on the Moon more than 33 hours and the landing crew will leave the spacecraft twice to emplace scientific experiments on the lunar surface and to continue geological investigations. The Apollo 13 landing site is in the Fra Mauro uplands; the two National Aeronautics and Space Administration previous landings were in mare or 'sea' areas, Apollo 11 in the Sea of Tranquility and Apollo 12 in the Ocean of Storms.
    Keywords: Lunar and Planetary Science and Exploration
    Type: NASA-News-Release-70-50K
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  • 7
    Publication Date: 2019-08-14
    Description: A summary of the scientific rationale for each Apollo landing site listed by the Group for Lunar Exploration Planning on February 7, 1970 is presented. These sites include the Fra Mauro Formation, Littrow, Censorinus, Davy crater chain, Marius Hills, Descartes, Tycho, Copernicus central peaks, and Hadley-Apennines. In addition, a summary of the scientific rationale for Flamsteed P, the Apollo 13 backup site, and Hyginus is presented.
    Keywords: Lunar and Planetary Science and Exploration
    Type: NASA-CR-109867 , B70-03034 , HQ-E-DAA-TN57955
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  • 8
    Publication Date: 2019-08-14
    Description: The Phase III analyses of Flight Research Facilities performed as a portion of the Hypersonic Research Facilities (HYFAC) Study are presented herein. Two attractive flight research vehicle concepts, geared to the development needs of future (1980-2n00) operational hypersonic aircraft systems, are defined. The inherent research capability of each concept is further expanded by incorporating provisions within the basic vehicle design to accommodate the testing of several additional research options. The design feasibility of this approach to achieving increased research flexibility is examined. Near term propulsion systems are employed as the basic power plants to shorten acquisition time, reduce development costs, and provide high confidence in attaining the performance capability desired, Performance is determined for each basic vehicle and for the vehicles when incorporating several optional research packages. Total program cost estimates are developed for each vehicle and for the various research options. This study provides the necessary framework for the formulation of an attractive and needed flight research program which is a key element in the systematic development of an overall advanced research plan.
    Keywords: Aircraft Propulsion and Power
    Type: MDC-A0013-VOL-4-PT-1-PHASE-3 , NASA-CR-114327
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  • 9
    Publication Date: 2019-08-24
    Description: Particle track densities up to greater than 3 x 10(exp 9) per square centimeter have been measured in different samples. Rocks 17, 47, 57, and 58 have VH (Z greater than 22) galactic cosmic ray ages of 11, 14, 28, and 13 x 10(exp 6) years, respectively. Rock 57 has a calculated erosion rate of approximately less than 10(exp -7) centimeter per year. Near-surface track versus depth data in rock 17 can be fit with solar flare particles that have a differential energy spectrum alpha E(exp -s); lunar samples can be used to study the history of solar activity. The uranium in the crystalline rocks occurs principally in small regions less than 10 to approximately equal to 100 micrometers in size. The (low) thermoluminescence of the fines increases with depth in core 10004. With one possible exception, x-ray studies have not shown pronounced radiation damage effects. The total energy release upon heating is small up to 900 C and occurs in three broad regions.
    Keywords: Lunar and Planetary Science and Exploration
    Type: Science; 167; 3918; 563-566
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  • 10
    Publication Date: 2019-07-13
    Description: Airbreathing hypersonic aircraft employing liquid hydrogen fuel have the potential of satisfying a number of mission requirements in the 1980-2000 time period. However, major advances in the technological state of the art are necessary before such aircraft can be considered either feasible or practical. The objective was to assess the research and development requirements for hypersonic aircraft and based on these requirements, to provide the NASA with characteristics of a number of desirable hypersonic research facilities. The study is organized in three phases. Phase I is a preliminary analysis of a broad group of concepts. The purpose of Phase I was to compare the characteristics of these facilities considering research capability, versatility, adaptability, system confidence and costs and based on these comparisons select those facilities that appear most attractive for parametric study and further refinement in Phase II. This part of Volume II presents the results of the design and cost synthesis of the flight research facilities.
    Keywords: Aircraft Propulsion and Power
    Type: NASA-CR-114324 , MDC-A0013-VOL-2-PT-2-PHASE-2
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