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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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Surface failure of titanium carbide cermet and silicon carbide ball in rolling contact at temperatures to 2,000-deg f
F region irregularities studied by scintillation of signals from satellites
Turbojet combustor and fuel system operation with hydrogen fuel at -400 deg F
Calculation of diffusion and drift velocities in nightime F region, and measurements of ion density in D-region of ionosphere
Miniature integrating gyro sterilization exposure studies at 300 deg F
Development of refractory metal alloys with high strength temperatures over 3000 deg F - extrusion at ultrahigh temperatures for 1020-ton vertical extrusion press
Ground support equipment and launch installations for manned lunar landing program at John F. Kennedy Space Center
IR and UV spectra of free radical FCO in argon matrix at cryogenic temperature of reaction of F atoms with CO
Modified, commercially available thermocouple which measures the temperature of a spacecraft heat shield, is capable of continuous measurement in the range of minus 250 deg to 5000 deg F. The modified thermocouples may be used inside metal treating furnaces in high temperature technology, and in certain corrosive environments.
Tensile properties of single crystal and polycrystalline tungsten from 2500 to 5000 deg F
Recursive computation of coefficients for time dependent f and g series solution to two-body problem of Keplerian motion
Stress rupture properties of tungsten wire from 1200 to 2500 deg F
F and K corona observations by rocket coronagraph during solar eclipse
Hydrogen thermal conductivity at temperatures from 2000 to 4600 deg F
Potassium condensing tests of horizontal multitube convective and radiative condensers operating at vapor temperatures from 1250 to 1500 degrees F
Recursive generation of expansion coefficients of time-dependent f and g series in two-body problem, using algebraic recurrence formulas
Extrusion of refractory metal alloys at 5000 degrees F
Thermal conductivity of hydrogen at temperatures up to 4700 degrees F determined indirectly from effective conductivity of porous tungsten specimens filled with pressurized hydrogen