Parametric reentry study of elliptic earth orbits with apogees up to 10,000 nautical miles
Mathematical model of parametric reentry study of elliptic earth orbits with apogees up to 10,000 nautical miles
Pruett, W. R.↗
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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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Integrated launch reentry vehicle configuration study
Tip tank configuration concept for integrated launch reentry vehicles
Stalony-Dobrzanski, J.↗
Turbulent heating on space shuttle orbiters during reentry
Turbulent reentry heating on delta wing and straight wing space shuttle orbiters
Hamilton, H. H.↗
Variable-geometry winged reentry vehicle Patent
Delta winged, manned reentry vehicle capable of horizontal glide landing at low speeds
Phillips, W. H.↗
Optimal three dimensional reentry trajectories for Apollo-type vehicles
Numerical optimization method based on perturbation theory for calculating optimal three dimensional reentry trajectories for Apollo type vehicles
Williamson, W. E., Jr.↗
Multistage multiple-reentry turbine Patent
Multistage, multiple reentry, single rotor, axial flow turbine
Evans, D. G.↗
Hypersonic reentry vehicle Patent
Aerodynamic configuration of reentry vehicle heat shield to provide longitudinal and directional stability at hypersonic velocities
Lamb, R. H.↗
Advanced evaluation of vacuum UV detector- spectroscopy systems for capsule reentry measurements
Vacuum ultraviolet detector evaluation - spectroscopy systems for capsule reentry measurements
Betz, H. T.↗
Reentry targeting philosophy and flight results from Apollo 10 and 11
Reentry targeting philosophy for Apollo missions emphasizing premission planning activities and real time targeting decisions, discussing Apollo 10 postflight results
Graves, C. A.↗
Reentry capsule dynamics
Blunt heat shield effectiveness for trailing payload in reentry capsules, discussing dynamic instability effect
Ericsson, L. E.↗
Atmospheric density models for reentry heating and trajectory applications
Upper stratosphere-mesosphere monthly-mean charts from reentry heating and atmospheric model based on hydrodynamics
Bowman, W. A.↗
Comparison of theoretical and flight-measured ionization in a blunt body reentry flow field
Plasma diagnostic data from onboard Langmuir probes, reflectometers, antenna VSWR and beacon and telemetry attenuation for blunt body reentry flow field
Evans, J. S.↗
Correlations of heat and mass transfer for the stagnation region of a reentry vehicle with multicomponent mass addition
Reentry vehicle with multicomponent gas mixture injection, calculating heat and mass transfer correlations for stagnation point flow
Curry, D. M.↗
Reentry communication by material addition Patent
Reentry communication by injection of water droplets into plasma layer surrounding space vehicle
Nelson, C. H.↗
Flight results of a 25000-foot-per-second reentry experiment using microwave reflectometers to measure plasma electron density and standoff distance
Comparing results of reentry plasma diagnostic experiment at 25,000 ft/sec with flow-field values at four locations on spacecraft
Grantham, W. L.↗
Apollo 7 retrofire and reentry of service propulsion module. Further study of Intelsat 2 F-2 apogee burn
Photography of Apollo 7 retrofire and service propulsion module reentry and apogee burn of Intelsat 2 F-2 satellite
Grandfield, M.↗
Overview of the AF Avionics Laboratory reentry electromagnetics program
Radio wave propagation through plasmas studied for communication with hypersonic vehicles during reentry
Robert Rawhouser↗
Reentry plasma measurements using a four frequency reflectometer
Hypersonic reentry plasma diagnostic measurements made with four-frequency microwave reflectometer
William L. Grantham↗