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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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Combination of temperature-compensated logarithmic amplifiers and p-i-n photodiodes operating in zero-bias mode provides lightweight radiometer for detecting spectral intensities encompassing more than three decades over a range of at least 300 to 800 nanometers at low power levels.
Handbook for structural stability analysis of sandwich structures under typical loading conditions encountered in aerospace applications
Structural analysis of glass filament wound, aluminum lined pressure vessel designs
Subthreshold electron irradiation effects on semiconductor surfaces
One dimensional solution of nonlinear waves of rate sensitive, elastoplastic material
Sliding friction and wear problems under unlubricated and boundary-lubricated conditions
High energy electromagnetic radiation and energetic particles from sun, galaxies, and nuclear explosions in spacecraft environment
Stress corrosion cracking tests for nickel steels
Hybrid microcircuit quality standards, inspection criteria, and reliability screening
Photovoltaic characteristics of p-n and n-p Si cells and p-n lithium-doped cells irradiated with high energy electrons
The Thorad-Agena is a two-stage launch vehicle consisting of a Thorad first-stage and an Agena second-stage, connected by a booster adapter. The composite vehicle, including the shroud and the booster adapter, is about 33 meters (109 ft) long. The total weight at lift-off is approximately 91 625 kilograms (202 000 lbm).
Project management in Apollo program
Cb-1Zr Rankine system corrosion test loop
Experimental windage losses for close clearance rotating cylinders in turbulent flow
High intensity heat and light unit containing quartz lamp elements protectively positioned to withstand severe environmental stress
Sonic boom simulation by low pressure sources
Computerized performance evaluation of Apollo thrust vector digital autopilot control system
Design criteria for spaceborne telescope structure