Feasibility study for a multiple satellite system. Volume I - Summary Final report
Multiple satellites in noncoplanar array used to define spatial and temporal variations of solar wind in interplanetary space
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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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Multiple satellites in noncoplanar array used to define spatial and temporal variations of solar wind in interplanetary space
Configuration, rod tradeoff, and deployment parameter studies for design of solar panel array
Nuclear magnetic resonance and nuclear quadrupole resonance techniques for nondestructive testing of reinforced plastics for curing and internal stresses
Rotating boiler for high performance Rankine cycle power generator using water as test fluid, obtaining heat-transfer coefficients
V/stol concepts for short haul commercial aircraft compared for gross weight, operating cost, gust sensitivity and noise levels
Wireless microwave or laser energy transfers power from a manned earth-orbiting central station to unmanned astronomical substations. More efficient systems are required for the microwave power transmission.
Design and volumetric analysis of pressurized tanks for use in liquid-methane fueled supersonic transport aircraft
Engineering design criteria for 30 watts per pound rollup solar array
Time division access system for satellite communications, and figure of merit for effects of bit and frequency synchronization
Fluid amplifier applications to gas cooled reactor rod control
Transient starting characteristics of small scale blowdown wind tunnel test facility
System dynamics and control analysis of tungsten water moderated nuclear rocket
Tensile strength and X ray analysis of resistance spot welded aluminum and stainless steel alloys
Dynamic structure and stress analysis of Scout launch vehicle with 44 inch ALGOL engine
Design criteria for five element folding arm used in roll-up solar arrays
Large space parabolic expandable truss antenna experiment
Parabolic expandable truss antenna experiment design for Apollo applications program
Altitude of orbiting spacecraft corrected by thrustor firing time control system