Factors affecting food development for space flight.
Food packaging and handling under zero-g conditions of space
WEIGHTLESSNESS↗
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Results for “Space Development”
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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Metallurgical evaluation of a new aluminum casting alloy developed for space vehicle use at cryogenic temperatures.
Metallurgical evaluation of aluminum casting alloy for high strength and toughness requirements for space vehicle use at cryogenic temperatures
SPACECRAFT CONSTRUCTION MATERIAL↗
Infrared spectrometer development for space vehicle study of planetary atmospheres Final report
Vibration and thermal radiation effects on filter wedge infrared spectrometer used in spacecraft studies of planetary atmospheres
PLANETARY ATMOSPHERE↗
Development of space launch facilities.
Manned lunar launch area site selection and planning, considering safety hazards, spaceport zoning, instrumentation, interference control, community relations, etc
LUNAR LAUNCH↗
Infrared spectrometer development for space vehicle study of planetary atmospheres annual report, 1 mar. 1964 - 28 feb. 1965
Explore the source record for details and available documents.
Pimental, G. C.↗
Space instruments development
Explore the source record for details and available documents.
Source record↗
Development of space stable thermal control coatings Triannual report, Mar. 1 - Jul. 31, 1967
Ultraviolet irradiation effects on space stable thermal control zinc coatings
Noble, G.↗
The development of space suit systems.
Space suits for Gemini and Apollo manned space programs, discussing life support system for proposed extravehicular excursions
Johnston, R. S.↗
Development of space stable thermal-control coatings Triannual report, 1 Oct. - 31 Dec. 1969
Thermal stability of protective coatings for large space vehicles
Ashford, N. A.↗
Development of space stable, low solar absorptance, pigmented thermal control coatings Final report, 17 Oct. 1968 - 16 Oct. 1969
Theoretical models and spectral reflectance measurements of white pigmented, low solar absorptance coatings for spacecraft temperature control
Brzuskiewicz, J.↗
Atmospheric electricity criteria guidelines for use in space vehicle development
Atmospheric electricity criteria guidelines for use in spacecraft design
Daniels, G. E.↗
Materials investigation and tests for the development of space compatible electrical connectors, phase 1 Final report, 1 Jun. - 30 Nov. 1970
Digital pulse optimization for space compatible electric connectors
Clark, D. E.↗
Development of space stable thermal control coatings Triannual report, 1 May - 30 Sep. 1970
Using zinc orthotitanate-pigmented potassium silicate paints for thermal control surface coatings
Zerlaut, G. A.↗
Materials investigation and tests for the development of space compatible electrical connectors Final report, 1 Jun. - 30 Nov. 1970
Selection of materials for electrical connectors compatible with future space missions
Johnson, C. A.↗
Design-development testing - Space vehicle design criteria
Criteria and procedures for testing spacecraft structural elements and components
Source record↗
Materials investigation and tests for the development of space compatible electrical connectors
A molding study of compounds based on copolymers of highly fluorinated olefins and of flame retardant silicone is reported. Both single cavity and four cavity molds having size 22 and 24 holes with three webs in each hole were used. Also covered are dielectric strength, arc resistance, Bashore rebound, and maintenance aging tests on the various materials that have been successfully molded.
Pomeroy, C.↗
Development of space stable thermal control coatings for use on large space vehicles
The evaluation and environmental testing of zinc orthotitanate pigments for use as space stable thermal control coatings on large space vehicles are discussed. Electron paramagnetic resonance spectra of the pigments and their precursor compounds are examined. A continuing study of the spectral intensity of mercury-argon and mercury-xenon sources in reported. Results of long term environmental testing of commercially available, strippable, protective coatings are discussed.
Gilligan, J. E.↗
Long range planning for the development of space flight emergency systems.
The importance of long-range planning for space flight emergency systems is pointed out. Factors in emergency systems planning are considered, giving attention to some of the mission classes which have to be taken into account. Examples of the hazards in space flight include fire, decompression, mechanical structure failures, radiation, collision, and meteoroid penetration. The criteria for rescue vehicles are examined together with aspects regarding the conduction of rescue missions. Future space flight programs are discussed, taking into consideration low earth orbit space stations, geosynchronous orbit space stations, lunar operations, manned planetary missions, future space flight vehicles, the space shuttle, special purpose space vehicles, and a reusable nuclear shuttle.
Bolger, P. H.↗