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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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Engineering and physiological considerations involved in selection and validations of artificial gaseous atmosphere for gemini and apollo missions
The NASA Manned Spacecraft Center has been actively involved in the direction and support of programs leading to the selection and validations of the atmosphere for forthcoming Gemini and Apollo missions. This paper discusses the engineering and physiologic considerations involved, describes the investigations to validate spacecraft atmospheres, and discusses the implications derived from the results of these investigations.
Lunar logistics vehicle variability of surface models and surface considerations
Design considerations for spin stabilized satellites with rigid expandable structures
Reliability considerations in design, assembly, and testing of Mariner IV power system
Design considerations of astronomical telescopes for lunar surface observation
Topological considerations and synthesis of linear networks by means of method of structural numbers
Aerospace medical and bioengineering considerations in M-2 lifting body research vehicle, discussing protective equipment, escape and medical monitoring systems
Two-electron spectra with consideration of four pure coupling types in study of energy level structure, relative line strengths and Lande g factors
Energy considerations in stability analysis of discrete linear structural systems under nonconservative forces
Design considerations for thermostatic fin spacecraft temperature control
Scientific satellite design considerations for spacecraft itself, spacecraft/launch vehicle interface, and ground support equipment and transportation
Meteorological considerations in handling liquid fluorine and liquid oxygen mixture
Viscoelasticity and plasticity considerations in fracture of glasslike high polymers
Basic considerations for DC to DC conversion networks, detailing relationship between characteristics of active resistor and maximum AC POWER generated by active element
Use of Jupiter gravity turns for tailoring trajectories to Saturn with consideration of launch opportunities
Design considerations for midcourse guidance and terminal descent system of Surveyor lunar soft landing spacecraft
Theoretical considerations on flow of blood through capillary