The oxidation and sublimation of graphite in simulated re-entry environments.
Graphite thermochemical response tested in simulated environment for use as thermal shield for hypersonic reentry vehicles
REENTRY SHIELD↗
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Results for “Re-Entry”
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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Hypersonic aerodynamic problems at re-entry of space vehicles
Hypersonic aerodynamic problems at space vehicle reentry - plasma effects on communications blackout, hypersonic flow, and atmospheric entry
PLASMA PHYSICS↗
Optimum earth re-entry corridors
Steepest ascent optimization procedure for reentry trajectory of manned aerospace vehicles
REENTRY TRAJECTORY↗
The oxidation and sublimation of graphite in simulated re-entry environments
Graphite oxidation and sublimation in simulated reentry environments
TEMPERATURE EFFECT↗
An experimental investigation of the re-entry behavior of metals and alloys
Oxidation and ablation behavior during simulated reentry of metals and alloys for use in NERVA REACTOR
REENTRY↗
The use of Langmuir probes to determine the electron density surrounding re-entry vehicles Final report
Langmuir probes for determining electron density surrounding reentry vehicles
REENTRY VEHICLE↗
A system for re-entry tracking of the Apollo spacecraft
Wide beam radio interferometer system for reentry tracking of Apollo spacecraft
APOLLO SPACECRAFT↗
Subsonic Aerodynamic Characteristics of Pyramidal Re-entry Shapes Incorporating Variable Geometry
Aerodynamic characteristics of pyramidal reentry shapes with variable geometry, at subsonic speeds
REENTRY BODY↗
Study of local flow conditions over a hemispherically blunted 25 deg cone for a shallow re-entry trajectory
Local flow conditions over hemispherically blunted 25 deg cone for shallow reentry trajectory
BLUNT BODY↗
Theoretical and Experimental Investigations of Spacecraft Antenna Problems in the Varied Operational Environments of Far-out-space and Atmospheric Re-entry Semiannual Report, 1 Jan. - 31 Jul. 1966
Spacecraft antenna, aperture, and reentry problems
ANTENNA↗
Re-evaluation of heat-transfer data obtained in flight tests of heat-sink shielded re-entry vehicles.
Stagnation point velocity and pressure distribution over heat-sink shielded reentry vehicle to test boundary layer heat transfer theories
HEAT SHIELD↗
Magnetoaerodynamic re-entry.
Entry flight, relation between laboratory flows, in-flight conditions and MGD effects on flow field, drag and heat transfer
FLOW FIELD↗
An alternate analysis of momentum deposition in the wake of a re-entry vehicle.
Momentum deposition in wake of reentry vehicle, discussing behavior of complex materials characterized by heat of ablation
MOMENTUM STORAGE↗
Including re-entry heating in rocket engine thermal analyses.
Reentry heat flux condition transformation into specified convective coefficients and temperatures, accounting for variation of flux with wall temperature
REENTRY CONDITION↗
A preliminary investigation of modified blunt 13 deg half-cone re-entry configurations at subsonic speeds
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REENTRY VEHICLE↗
The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90
Aerodynamic characteristics of blunt, lifting body reentry configuration
AERODYNAMIC CHARACTERISTICS↗
A Method for Determining Optimum Re-entry Trajectories
Determining optimum atmospheric reentry trajectories using Pontryagin maximum principle
PONTRYAGIN PRINCIPLE↗
Use of the Langmuir probe to determine the electron density and temperature surrounding re-entry vehicles Final report
Shock tube tests of Langmuir probe for determining electron density and temperature surrounding reentry vehicle
ELECTRON DENSITY↗