Telecoupled impacts of livestock trade on non-communicable diseases
Explore the source record for details and available documents.
SEARCH · Search NASA
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
The purpose of this paper is to examine the mission capability of hydrogen-fueled hypersonic transports and to discuss some of the major technical approaches that may be used with such vehicles . It is the intention of this paper to indicate only the technical feasibility and capabilities of hypersonic transports. The equally important problems involving economic feasibility and operational problems have not been considered, since the study of these problems is thought to be premature until technical feasibility has been established.
Economic analysis of retail business in Cape Kennedy area
Parametric evaluation of hydraulic, pneumatic, and electromechanical actuators for manned spacecraft tasks
Weight-area tradeoff evaluation of radiator used in SNAP-8
Parametric and procedural tradeoffs for alignment and calibration of inertial sensing unit
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Technologies and design concepts of closed integrated life support system for prolonged manned space flight mission
Computerized tradeoff analysis for planetary landing vehicle entry capsule and lander design optimization, emphasizing weight allocation for Mars 1973 missions
Pulse compression for geodesy satellite radar altimeter, considering tradeoff based on system accuracy, power and life
System analysis and computer requirements derivation of guidance and control computer for space station applications - Vol. 5
Booster wing geometry effects on space shuttle design requirements
Environmental control and life support subsystem for space shuttle orbiter
Computer requirements of self contained guidance, navigation and control system onboard manned orbital space station
Canard space shuttle reusable launch vehicle wing geometry variations effect on flyback systems weight, noting influence of aspect ratio and wing area