Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed
Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parabolic speed
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Aerodynamic heating of conical vehicles entering earth atmosphere at speeds greater than earth parabolic speed
Space vehicle structural design for ascent, space flight, and reentry
Manned lunar return launch and reentry vehicles, emphasizing spacecraft and system weight in relation to mission mode and propulsion
Characteristics of air at high temperatures for consideration in design of reentering space vehicles
Principles for determining properties of unknown planetary atmosphere from responses of reentering probe vehicle
Langmuir probes for determining electron density surrounding reentry vehicles
Stagnation point velocity and pressure distribution over heat-sink shielded reentry vehicle to test boundary layer heat transfer theories
Momentum deposition in wake of reentry vehicle, discussing behavior of complex materials characterized by heat of ablation
Weight estimates of thermal protection systems for lifting body reentry vehicle suitable for near earth missions
Shock tube tests of Langmuir probe for determining electron density and temperature surrounding reentry vehicle
Lateral directional handling qualities of piloted reentry vehicles utilizing fixed base and in flight evaluations
Heat transfer measurements on rotor blade of reentry vehicle model
Modified control logic with random-number procedure to determine error effects on range controller of reentry vehicle
Aerodynamic and performance characteristics of unpowered rotor reentry vehicle
Environmental and ablative materials performance affecting heat shielding requirements of slender and blunt vehicles during hyperbolic reentry
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry vehicles
RF/plasma interactions relative to reentry plasma diagnostics and microwave transmission, noting increased hot air susceptibility to RF breakdown
Operating and aerodynamic characteristics of rotor in autorotative flight analyzed for reentry from orbit