Traction drive system design considerations for a lunar roving vehicle
Optimum design considerations of traction drive for lunar roving vehicle
Doran, B. J.↗
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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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Design considerations and requirements for integrating an electric propulsion system into the SERT 2 and future spacecraft
Design considerations and requirements for integrating electric propulsion systems into SERT 2 and future spacecraft
Rulis, R. J.↗
Transient loading considerations for shuttle design
Transient loading considerations for shuttle design
Baird, E. F.↗
Minitrack postdetection bandwidth considerations
Design considerations for phaselock loop response of postdetection filter in Minitrack system
Grenchik, T. J.↗
Some trim drag considerations for maneuvering aircraft
Aft tail and canard configurations trim drag considerations for maneuvering aircraft
Dollyhigh, S. M.↗
Fundamental design considerations for an earth-surface-to-orbit shuttle
Reusable earth surface-to-orbit shuttle, discussing cost and performance design considerations
Faget, M. A.↗
Guidance and control considerations for advanced manned space missions
Guidance and control considerations for advanced manned space missions
Gardiner, R. A.↗
Lubrication considerations in gear design
Lubrication considerations in design of gears
Townsend, D. P.↗
Preliminary vibration design and test criteria considerations for the space shuttle
This paper presents some Marshall Space Flight Center preliminary vibration design and test criteria considerations for the space shuttle. The discussion is primarily concerned with the formulation of vibration criteria for the design and testing of the equipment installations on the shuttle. A recommended criteria format is presented with a discussion of when the vibration environment has to be considered in design and testing. A semiempirical method of predicting the vibration criteria for the shuttle from vibroacoustic structural data banks is presented. Some preliminary vibration criteria predictions are presented for the orbiter and booster equipment bays and for the main shuttle engine. A research testing program to determine the vibroacoustic transfer through a typical shuttle thermal protection system (TPS) panel configuration is described.
Harry J. Bandgren↗
Investigation of the solidification, structure and properties of eutectic alloys including consideration of properties control
Solidification, structure, and properties of eutectic alloys including consideration of properties control
Kraft, R. W.↗
Program on application of communications satellites to educational development. An instructional satellite system for the United States: Preliminary considerations
Audio-Visual Satellite Instruction system (AVSIN) for USA - preliminary considerations
Dumolin, J. R.↗
Lubrication considerations in gear design
Lubrication considerations concerning mechanical and service variables for obtaining optimum gear performance under severe operating conditions
Townsend, D. P.↗
Design considerations for Gardon heat flux sensors
Centerline loss, transient sink temperature and thermal conductivity design constantan considerations for thin foil copper-Gardon heat flux sensors
Ash, R. L.↗
A space shuttle design consideration
Earth-to-orbit space shuttle booster and orbiter unit design considerations including low development cost, risk and time, weight and payloads
Peterson, C. B.↗
Nuclear safety considerations for manned space flight
Nuclear safety considerations for ground checkout, launch and in-orbit operations of reactors for earth orbital manned space stations
Gerrels, E. E.↗
Radioisotope thermoelectric generator safety and operations considerations for users of large nuclear space power systems
Radioisotope thermoelectric generator safety and operations considerations for users of large nuclear space power systems
Weber, W. B.↗
Design considerations for combined radiation effects facilities for twelve year outer planet spacecraft voyages
The design considerations influencing the choice and utility of environmental simulation methods and facilities are described, insofar as they relate to the requirements imposed on outer planet spacecraft because of radiation environments to be expected. Possible means for duplicating the radioisotope thermoelectric generator radiation environment, and for duplicating the effects of the trapped radiation belt environment are described, together with an assessment of radiation levels to be expected in the vicinity of an environmental testing chamber when in use.
Miller, C. G.↗
Recovery considerations for possible high inclination long duration earth orbital missions
Problem areas are discussed and various solutions proposed. One of the major recovery problems encountered with missions having higher orbital inclinations than previous missions is the greater likelihood of severe weather conditions in the landing zones, especially if landing zones are optimized for orbital coverage considerations. Restricting the reentry window and increasing in-orbit wait times can partially eliminate the weather problem, but the possibility of emergency landings at higher latitudes still exists. It can be expected that the increased confidence level in spacecraft reliability that will exist by the time the high-inclination missions are flown will reduce the probabilities of an emergency landing in an unfavorable recovery location to a very low level.
Obriant, T. E.↗