Development of a prototype plastic space erectable satellite Quarterly report, Dec. 1965 - Feb. 1966
Plastic space erectable satellite
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Plastic space erectable satellite
Capacitive mass flow meter with electronic readout for use with liquid hydrogen
Respiration analyzer for in-flight monitoring of human respiratory functions
Dynamic lateral stability and handling data from flight simulation with F6F-3 and F-86A VARIABLE-STABILITY aircraft
Copper plated high-density polyethylene film evaluation for space erectable satellite design
Tools for induction brazing of stainless steel tubing and fittings
Fabrication of high temperature silicon carbide integrated circuit using junction-gate type field effect transistor as active component
Refractory bimetallic tubing bond quality testing by metallographic and ultrasonic inspection
Human reaction to operation of document search and retrieval system
Performance of thermionic converters, discussing voltage output, interelectrode spacing, rhenium- rhenium and rhenium-molybdenum electrode systems
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Thermal energy storage container integration with thermionic converter
Design criteria and mathematical model for vapor diffusion water reclamation unit
Pulsed ruby laser satellite tracking system
Decomposition temperature of monomeric azines relation to electronic nature of R substituent, contributing resonance structures and hydrogen bonding
Portable lighting system serves the combined work and photographic needs of manned spacecraft efforts. This system enables the lamps to be momentarily brightened while the camera shutter is opened. The brightness is adequate for black and white or color photography and yet the increased heat load is nil.
Mobility and restraint device employing shuffling technique for space station environments
Monolithic amplifier incorporating vertical n-p-n and lateral p-n-p transistor structures