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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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Electron energy effects on reflectance degradation and recovery of thermal control materials in vacuum, reporting test results for various protective coatings
Investigation into the uses of step-recovery diodes /SRD's/ leads to the development of necessary circuitry for using fast current-switching capabilities of SRD's in frequency multiplication, the design of solid-state X-band transmitters employing SRD multipliers, and the use of SRD multipliers in a phased-array receiving antenna.
Microorganism recovery from pulverized and leached solid rocket propellants and spacecraft components
Step recovery diode multipliers to control phase of microwave phased array antenna systems
Performance evaluation of evaporative water recovery subsystem utilizing automatic feed control
Mechanisms of recovery of radiation damaged silicate treated zinc oxide thermal control coatings
Wind tunnel characteristics of ejection seat scale model with rigid wing recovery system
Integrated temperature and humidity control and water recovery subsystem for manned test in space station simulator
Suboptimum sequential algorithm for recovery decoding errors in convolutional codes, using Hamming distance criterion
Phase recovery and calibration techniques for position location interferometer in synchronous orbit
Development and characteristics of hot air balloon deceleration and recovery system
Failure analysis of recovery flasing xenon lamp on Apollo 10 flight
Diagnosability and recovery from massive faults in digital systems
GEOSTAR-2 multiple arc geopotential coefficient and station position recovery system
System and component design and development for intermediate water recovery system for 3-man, earth orbital spacecraft on 1-year mission
Component specifications and computer program for intermediate water recovery system on manned spacecraft
Aerobee 350 recovery system comprising paraloon and extended skirt parachute deceleration devices and incorporating electrical control, pyrotechnic, and pneumatic subsystems - tests
GEOS-3 altimeter bias recovery simulation using range and angle tracking data