Force feeding on the response of japanese quail to oxygen toxicity.
Food intake and oxygen toxicity in quail, cortrunix japonica
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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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Food intake and oxygen toxicity in quail, cortrunix japonica
Photographs and mosaics of lunar surface obtained from Surveyor 6
Variational methods for determining optimum design and flight of rockets
Lunar topological photography from Surveyor 7 mission
Tuft-grid photographic survey of flow field about low speed delta wings
Surveyor spacecraft instrumentation, describing TV camera design and operation, photographic requirements and techniques, lunar surface characteristics, etc
White mice gastrocnemius muscle wet mass, dry mass and noncollagen-nitrogen /NCN/ content, noting /NCN/ content dependence on body mass
Gas laser iterative alignment of Mach-Zehnder interferometer for monochromatic and white light fringes
Tranquillity Base lunar soil origin, establishing component nature, size distribution, density, mineralogy, constructional or destructional history
Dosimeter determines time-integrated radiation dosage to which an individual is exposed. Integration is measured chemically in proportion to radiation detected. Wearer receives an exposure measurement representing an average of the dose over the entire body.
Iterative technique using continuous gas laser for alignment of Mach-Zehnder interferometer for monochromatic and white light fringes
Petrography, mineral composition and grain size distribution of Apollo 12 lunar fines
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This paper studies the feasibility of the use of an atmospheric rendezvous concept to increase the efficiency and flexibility of space transportation systems. In this concept the second stage of a recoverable orbital launch vehicle or hypersonic transport would be built without wings, landing gear, or subsonic flight propulsion, and would be received in an atmospheric rendezvous by a carrier vehicle at the terminal point of flight for subsequent ferry to a landing site. Significant possibilities for weight improvement are shown and the attractiveness of a subsonic form of atmospheric rendezvous in either a towing or docking mode is illustrated.
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