Radar cross section and optical radiation from the Trailblazer IIa 9 deg half-angle blunt nose cone during hypersonic reentry
Radar cross sections and optical radiation measurement of blunt nose cone during hypersonic reentry
HYPERSONIC REENTRY↗
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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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Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects
Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach numbers, including Reynolds number effect
AERODYNAMIC CHARACTERISTICS↗
An evaluation of free-flight test data for aerodynamic heating from laminar, turbulent, and transitional boundary layers. Part II - The X-17 reentry body
Blunt body reentry vehicle aerodynamic heating determination
REENTRY VEHICLE↗
Angle-of-attack analysis for Project Fire 1 payload reentry flight
Computer program for Project Fire 1 payload reentry flight angle of attack analysis
ANGLE OF ATTACK↗
Study of aerothermodynamic phenomena associated with reentry of manned spacecraft Final report, Nov. 1964 - May 1966
Aerothermodynamic phenomena associated with reentry of manned spacecraft
AEROTHERMODYNAMICS↗
Development of Ablation Sensors for Advanced Reentry Vehicles
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal parameters of ablative reentry vehicle heat shield
ABLATING MATERIAL↗
Infrared Sensor for Apollo Reentry Final Report, 1 Jul. - 30 Dec. 1964
Infrared sensor used to augment radio frequency tracking during Apollo vehicle reentry into earth atmosphere
RADIO FREQUENCY↗
Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack up to 90 Degrees
Stability and control characteristics of reentry vehicle configurations at angles of attack up to 90 deg, in wind tunnel at Mach number 2.91
STABILITY AND CONTROL↗
Transonic static and dynamic longitudinal stability characteristics of a low-fineness- ratio, blunted-cylinder reentry body having a converging-cone afterbody
Transonic static and longitudinal stability characteristics of low fineness ratio, blunted cylinder reentry body with converging cone afterbody
BLUNT BODY↗
Stability and control characteristics at a Mach number of 1.89 of a lightweight glider reentry configuration
Stability and control characteristics at supersonic speeds of lightweight reentry glider with diamond-wing planform
WING PLANFORM↗
NASA to launch 5th Scout reentry heat experiment
Scout vehicle flight experiment to determine performance of phenolic nylon spacecraft heat shield material under reentry conditions
ABLATING MATERIAL↗
Navigation accuracy for infrared equipped Apollo aircraft for reentry tracking
Navigational accuracy of infrared acquisition and tracking system for Apollo reentry aircraft
INFRARED TRACKING↗
Analytical Investigation of the Reentry Behavior of the ''flying Wind Tunnel'' Test Vehicle, with Some Effects of Threshold and Torque Level of a Roll-rate Control System
Analytical investigation of reentry behavior of flying wind tunnel test vehicle with some effects of threshold and torque level of roll-rate control system
CONTROL SYSTEM↗
High-altitude atmospheric measurements for the reentries of Gemini 6 and Gemini 7
High-altitude atmospheric measurements for reentries of Gemini 6 and Gemini 7
ATMOSPHERIC COMPOSITION↗
Atmosphere reentry guidance - Return from the manned Mars mission.
Reentry guidance for manned Mars mission return considering capture and acceleration control, skip range and terminal range controls
ATTITUDE CONTROL↗
Development of ablation sensors for advanced reentry vehicles.
Make wire, light pipe and spring wire ablation sensors development for measuring parameters of heat shield materials for reentry vehicles
MEASURING APPARATUS↗
Free-flight aerodynamics of a blunt-faced reentry shape with and without ablation.
Hypersonic aerodynamic stability and drag of ablating and nonablating models of blunt-faced reentry shape
BLUNT BODY↗
A summary of light-intensity data of eight Trailblazer I reentry bodies
Light intensity data of Trailblazer I reentry bodies
LIGHT INTENSITY↗