Plasma effects on apollo re-entry communication
Plasma effects on electromagnetic wave propagation during Apollo spacecraft reentry from lunar missions
APOLLO SPACECRAFT↗
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Results for “Reentry”
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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The nasa-lrc telespectrograph test and opera- tion results
Tracking telespectrograph for film record of reentry vehicle spectrum light - test and operation results
REENTRY VEHICLE↗
Luminous efficiency of an artificial meteor at 11.9 kilometers per second
Trailblazer II reentry vehicle artificial meteoroid experiment consisting of reentering 2.2-gram stainless steel pellet into earth
TRAILBLAZER II REENTRY VEHICLE↗
Apollo entry tracking- a shipboard unified s-band interferometer system
Apollo spacecraft reentry tracking with shipboard unified S-band interferometer system
SPACECRAFT TRACKING↗
A maximum principle re-entry study
Mathematical model of maximum principle of Pontryagin used to find point-to-point reentry trajectory of space vehicle
REENTRY TRAJECTORY↗
Pilot re-entry guidance and control
Operational problems of manually guided and controlled reentry vehicles
OPERATIONAL PROBLEM↗
Aerodynamic drag and stability.
Aerodynamic force and moment effect on performance of spacecraft during launch and reentry
DRAG↗
Structural loads.
Structural loads calculated for launch and reentry vehicles, noting extra loads due to system failures
REENTRY VEHICLE↗
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
WEIGHT FACTOR↗
Heat-shield ablation and sublimation determinations through radioisotope techniques.
Heat-shield sublimation and ablation determination during atmospheric reentry, using radioactive technique
ABLATION↗
Lorentz drag - an engineering approximation.
Method estimating relative magnitude of magnetoaerodynamic drag/MADD/ or Lorentz drag used for decelerating space vehicle reentry
MAGNETOHYDRODYNAMIC FLOW↗
Shock tube instrumentation techniques for study of hypervelocity entry problems.
Shock tube instrumentation to study convective and radiative heat transfer of hot gases simulating hypervelocity reentry
CONVECTIVE HEAT TRANSFER↗
The gemini program.
Gemini program - advances in operational capability during flight, rendezvous, extravehicular operations and reentry
GEMINI PROJECT↗
Translational and rotational motion of a body entering the Mars atmosphere
Translational and rotational motion of spherical body entering Mars atmosphere - reentry physics
SPHERE↗
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↗
Radar tracking ship performance during MA-9
Radar tracking ship performance during Faith 7 - Mercury /MA-9/ flight and evaluation for critical reentry tracking and manned space flight applications
RADAR TRACKING↗
Optimum earth re-entry corridors
Steepest ascent optimization procedure for reentry trajectory of manned aerospace vehicles
REENTRY TRAJECTORY↗
Determination of heat-shield char-front recession with a nucleonic technique
Radionuclide method for determining Apollo heat shield char-front recession during reentry
RADIOACTIVE NUCLIDE↗