A neighboring optimum feedback control scheme based on estimated time-to-go with application to re-entry flight paths.
Neighboring optimum feedback control scheme based on estimated time-to-go applied to reentry flight paths
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Neighboring optimum feedback control scheme based on estimated time-to-go applied to reentry flight paths
Apollo Command Module aerodynamics at reentry altitudes simulated by models in hypersonic flow
Interplanetary magnetic field reconnection at tangential discontinuities, discussing coincidence with proton temperature maxima in solar wind during magnetic storm
De Sitter hydrostatic theory of earth figure modified to make equations independent of external potential theory in calculating flattening
MGD during reentry, reviewing shock standoff, electromagnetic drag, heat transfer, laboratory reentry simulation and on-board magnet in reentry vehicle
Reynolds and Mach numbers simulation of Apollo and Gemini reentry compared with flight data
Separation system for two spinning bodies on atmospheric reentry trajectory
Mission planning manual on reentry turbulent heating experiment and spacecraft
Microwave radiometric techniques for reentry plasma measurements
Measurement of thermal accommodation coefficients between liquids and high temperature gases in low pressure reentry communications blackout intervals
Porous ceramic heat shields for lifting reentry vehicles, noting crack propagation resistance and load redistribution
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry
Surface climatological information for reentry ground stations
Electrostatic modulator for communicating through plasma sheath formed around spacecraft during reentry
Ablation of heat shielding materials subjected to superorbital reentry conditions, noting dependence on heating rate to surface
Model for magnetic field-line reconnection in conducting incompressible fluid, determining maximum reconnection rate entirely by null point conditions
Electron density reduction in plasma surrounding reentry vehicle due to N atom removal by water droplets injection
Electron concentration profiles in blunt nose vehicle shock layer during atmospheric near orbital entry at high altitudes, using finite rate chemistry