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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 163 records · Page 9
All sourcesNASA NTRSDOE OSTI
NASA NTRS1970

The Surveyor shock absorber

Surveyor spacecraft landing shock absorbers design and performance assessment by digital computer simulation

Sperling, F. B.↗
NASA NTRS1971

Microbial burden prediction model program

Model supplements biological surveys of spacecraft by simulating microbial burden accumulation process during periods when surveys are not taken. Important application of model is to predict microbial loading on spacecraft landing capsule immediately prior to terminal heat sterilization.

Meuser, R. F.↗
NASA NTRS1972

Evaluation of microbial release probabilities

Work undertaken to improve the estimation of the probability of release of microorganisms from unmanned Martian landing spacecraft is summarized. An analytical model is described for the development of numerical values for release parameters and release mechanisms applicable to flight missions are defined. Laboratory test data are used to evolve parameter values for use by flight projects in estimating numerical values for release probabilities. The analysis treats microbial burden located on spacecraft surfaces, between mated surfaces, and encapsulated within materials.

Source record↗
NASA NTRS1972

STDN network operations procedure for Apollo range instrumentation aircraft, revision 1

The Apollo range instrumentation aircraft (ARIA) fleet which consists of four EC-135N aircraft used for Apollo communication support is discussed. The ARIA aircraft are used to provide coverage of lunar missions, earth orbit missions, command module/service module separation to spacecraft landing, and assist in recovery operations. Descriptions of ARIA aircraft, capabilities, and instrumentation are included.

Vette, A. R.↗
NASA NTRS1974

Assessment of the probability of contaminating Mars

New methodology is proposed to assess the probability that the planet Mars will by biologically contaminated by terrestrial microorganisms aboard a spacecraft. Present NASA methods are based on the Sagan-Coleman formula, which states that the probability of contamination is the product of the expected microbial release and a probability of growth. The proposed new methodology extends the Sagan-Coleman approach to permit utilization of detailed information on microbial characteristics, the lethality of release and transport mechanisms, and of other information about the Martian environment. Three different types of microbial release are distinguished in the model for assessing the probability of contamination. The number of viable microbes released by each mechanism depends on the bio-burden in various locations on the spacecraft and on whether the spacecraft landing is accomplished according to plan. For each of the three release mechanisms a probability of growth is computed, using a model for transport into an environment suited to microbial growth.

Judd, B. R.↗
NASA NTRS1976

Mission description

The Apollo Soyuz mission was the first manned space flight conducted jointly by two nations. The United States and the U.S.S.R. achieved a substantial degree of success in: (1) obtaining flight experience for rendezvous and docking of manned spacecraft and developing a docking system that would be suitable for use as a standard international system, (2) demonstrating in-flight intervehicular crew transfer, and (3) conducting a series of science and applications experiments. The Apollo and Soyuz spacecraft, with minor exceptions, were similar to those flown on previous missions, but a new Apollo module, the docking module, was built specifically for this mission. The mission started with the Soyuz launch on July 15, 1975, followed by the Apollo launch on the same day. Docking of the two spacecraft occurred on July 17, and joint operations were conducted for 2 days. Both spacecraft landed safely and on schedule; the Soyuz landing in the U.S.S.R. occurred on July 21, and the Apollo landing near Hawaii occurred on July 24. Twenty-eight science experiments were performed during the mission.

Hardee, S. N.↗
NASA NTRS1977

Apollo-Soyuz pamphlet no. 1: The flight

The goals of the Apollo-Soyuz Test Project are described in this first in a series of nine pamphlets designed as a curriculum supplement for teachers, supervisors, curriculum specialists, and textbook writers as well as for the general public. Aspects of the space flight covered include descriptions of the astronaut-cosmonaut meeting and of the spacecraft and landing module; spacecraft launch; control, and rendezvous; crew work schedule; and telemetry. Experiments performed are listed in tables, and their major results are summarized.

Page, L. W.↗
NASA NTRS1977

Exploration of the planets - An invited discourse presented before the Sixteenth General Assembly of the International Astronomical Union, Grenoble, France, August, 1976

The paper reviews in situ observations of Venus, Jupiter, and Mars by various spacecraft, including Mariner 2, 9, and 10, Pioneer 10 and 11, Venera 8, 9, and 10, and Viking. Detailed attention is given to the Viking mission, emphasizing adaptive aspects of the Viking spacecraft, landing sites, instruments, the geology of Mars, measurements of atmospheric constituents, the nature of rocks and sediment, and the biology experiments. It is noted that the organic-chemistry experiment has yielded entirely negative results, while two of the three microbiological experiments have yielded positive results. It is concluded that at the very least, a nonbiological chemistry on the Martian surface has been found which duplicates many of the essential steps in animal respiration and in green-plant photosynthesis.

Sagan, C.↗
NASA NTRS1985

Permafrost and Subsurface Ice in the Solar System

The properties and behavior of planetary permafrost are discussed with reference to the ability of such surfaces to sustain loads characteristics of spacecraft landing and planetary bases. In most occurrences, water ice is in close proximity to, or in contact with, finely divided silicate mineral matter. When ice contacts silicate mineral surfaces, a liquid-like, transition zone is created. Its thickness ranges from several hundred Angstron units at temperatures near 0 degrees C to about three Angstrom units at -150 degrees C. When soluble substances are present, the resulting brine enlarges the interfacial zone. When clays are involved, although the interfacial zone may be small, its extent is large. The unfrozen, interfacial water may amount to 100% or more weight at a temperature of -5 degrees C. The presence of this interfacial unfrozen water acts to confer plasticity to permafrost, enabling it to exhibit creep at all imposed levels of stress. Nucleation processes and load-bearing capacity are examined.

Anderson, D. M.↗
NASA NTRS1985

Analyses of Radar Images of Small Craters

Clouds hide the surface of Venus from all but radar imaging systems, supplemented by limited views from land spacecraft. Among the surfaces features likely to be observed by radar are craters that have formed by a variety of processes. In order to assess the radar characteristics of craters, volcanic craters and impact structures on Earth are described as imaged by the Shuttle Imaging Radar (SIR-A) experiment. Although most of the craters are small, this analysis provides insight into the ability to discriminate craters of various origins and provides some basis for interpreting radar images returned from Venus.

Greeley, R.↗