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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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Design of calorimeters to obtain flight data at lunar reentry velocity and equations to convert telemetered temperature responses into heat flux valves
Atmospheric reentry guidance and control methods - bibliography
Derivation of three-dimensional three-degree-of- freedom reentry equations of motion in terrestrial navigational coordinates
Minimum drag atmospheric reentry trajectory for space vehicle with offset center of gravity
Traveling wave tube in reentrant mode for frequency conversion & amplification serrodyne system
Reentry heating experiment to be flown by scout launch vehicle to test ablating materials for use in apollo project flight
Missile data storage system for obtaining reentry heating data, employing ferrite memory and digital and analog circuitry
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Influence of age-associated changes in older pilots during relearning of aviation technology and during performance
Magnetic field interaction with hypersonic flow to effect deceleration and heating during reentry
Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at hypersonic speeds
Variations in signal levels received by radio interferometer system for various trajectories and altitudes of reentering Apollo command module
Thermionic work function of refractory metallic compounds and electronic and crystal structure - emissivity measurement and diode fabrication
Plasma effects on electromagnetic wave propagation during Apollo spacecraft reentry from lunar missions
Input bandpass filter, limiter, conventional and phase lock FM detector, output low pass filter, and offset frequency for FM receiver
Mathematical model of maximum principle of Pontryagin used to find point-to-point reentry trajectory of space vehicle
Operational problems of manually guided and controlled reentry vehicles