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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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Simultaneous magnetic field variations at earth surface and at synchronous equatorial distance, using ATS-1 magnetometers
Fractionation of distance in space environment simulation
Calculated aircraft stopping distances based on test results
Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies
Upper and lower bounds for feedback decoding and definite decoding minimum distances of binary convolutional codes
Interrelations of perceived size and distance
Heitler-London wave functions used to determine internuclear distance and velocity of electron exchange in H-H collisions
Time dependent variations in sky emission temperature, anomalous sky temperature variation with zenith distance on calm nights, lunar linear polarization - millimeter wavelengths
Space simulator to produce visual properties of objects outside earth atmosphere and determine distance and rate perception
Distance discrimination experiment in reduced cue setting simulating outer space, confirming Weber power function exponent
Opening distance and inflation time prediction for parachutes deployed supersonically based on subsonic performance
Correlation distance of VHF fading from irregularities in equatorial ionosphere, using NASA STADAN in Chile
Unit distance redundant counting code for single error correction or double error detection with digital equipment simplicity advantages
Heitler-London curves calculation for electron exchange in H-H collisions as function of internuclear distance and velocity
Analysis of multiple earth bow shock crossings at large geocentric distances from Pioneer 8 magnetic field data
Cyclic arithmetic codes and their distance properties with demonstration of modular arithmetic weight invariance to code word cyclic shifts
Wind tunnel tests to determine flow patterns and pressure distributions around bluff afterbody in wake of 120 deg cone for various separation distances at Mach 3.0
Least square distance curve fitting method