Return launch and re-entry vehicles.
Manned lunar return launch and reentry vehicles, emphasizing spacecraft and system weight in relation to mission mode and propulsion
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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
1924 and 1926 oppositions of Mars in W.H. Wright plates noting Mars diameter in IR AND UV
Reentry vehicle configuration from manned Mars missions, using aerobraking
Aerodynamic and structural aspects of rotary atmospheric entry aids, including high temperature rotor material selection, rotor blade design, and lift and drag modulation problems
Graphite thermochemical response tested in simulated environment for use as thermal shield for hypersonic reentry vehicles
Hypersonic aerodynamic problems at space vehicle reentry - plasma effects on communications blackout, hypersonic flow, and atmospheric entry
Steepest ascent optimization procedure for reentry trajectory of manned aerospace vehicles
Graphite oxidation and sublimation in simulated reentry environments
Reevaluating flow initiation systems for large tube wind tunnel
Oxidation and ablation behavior during simulated reentry of metals and alloys for use in NERVA REACTOR
Langmuir probes for determining electron density surrounding reentry vehicles
Wide beam radio interferometer system for reentry tracking of Apollo spacecraft
Aerodynamic characteristics of pyramidal reentry shapes with variable geometry, at subsonic speeds
Local flow conditions over hemispherically blunted 25 deg cone for shallow reentry trajectory
Spacecraft antenna, aperture, and reentry problems
Entry flight, relation between laboratory flows, in-flight conditions and MGD effects on flow field, drag and heat transfer
Spacecraft transponder with reentrant mode TWT AMPLIFIER