FREE-FLIGHT TESTS TO A MACH NUMBER OF 1.5 OF SLENDER TRIANGULAR PYRAMID REENTRY CONFIGURATIONS
Free flight tests of lifting surface reentry vehicles at mach 0.6 to 1.5
REENTRY VEHICLE↗
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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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A LOOK AT THE REENTRY PROBLEM
Optimal trajectory and physical parameters for reentry from earth orbits and space
REENTRY TRAJECTORY↗
Determination of trajectory and angles of attack of a scout heat-transfer spacecraft during reentry flight in the atmosphere
Unknown trajectory and angles of attack of Scout heat transfer spacecraft during reentry flight in atmosphere
ANGLE OF ATTACK↗
Photometric analysis of spectrograms of two Trailblazer I payload reentry events
Photometric analysis of spectrograms of two Trailblazer I payload reentry events
TRAILBLAZER I REENTRY VEHICLE↗
A simple atmosphere reentry guidance scheme for return from the manned Mars mission
Atmosphere reentry guidance scheme for return from manned Mars mission
REENTRY GUIDANCE↗
Static stability and control characteristics of two large-dihedral right triangular pyramid lifting reentry configurations at a Mach number of 3.05
Static stability and control characteristics of dihedral right triangular pyramid lifting reentry vehicle configurations
REENTRY VEHICLE↗
Rapid estimates of stability derivatives for reentry vehicles by rheoelectric analogy.
Rheoelectric analogy using apparent mass to obtain static and dynamic stability derivatives for lifting-body reentry vehicles
STABILITY DERIVATIVE↗
A study of ballistic reentry trajectories at a velocity of 50 000 feet per second /15 240 meters per second/
Ballistic reentry trajectories at hypersonic speed
HYPERSONIC REENTRY↗
Structures and materials for manned reentry vehicles.
Structures, materials and thermal protection systems for future manned reentry vehicles, emphasizing crew compartment compatible materials
STRUCTURAL MATERIAL↗
Landing Energy Dissipation for Manned Reentry Vehicles
The film shows experimental investigations to determine the landing-energy-dissipation characteristics for several types of landing gear for manned reentry vehicles. The landing vehicles are considered in two categories: those having essentially vertical-descent paths, the parachute-supported vehicles, and those having essentially horizontal paths, the lifting vehicles. The energy-dissipation devices include crushable materials such as foamed plastics and honeycomb for internal application in couch-support systems, yielding metal elements as part of the structure of capsules or as alternates for oleos in landing-gear struts, inflatable bags, braking rockets, and shaped surfaces for water impact.
REENTRY VEHICLES↗
AERODYNAMICS OF TRAJECTORY CONTROL FOR REENTRY AT ESCAPE SPEED
Aerodynamics of trajectory control for reentry at escape speeds
TRAJECTORY CONTROL↗
STATIC STABILITY INVESTIGATION OF PROPOSED PROJECT FIRE SPACE-VEHICLE AND REENTRY-PACKAGE CONFIGURATIONS AT MACH NUMBERS FROM 1.47 TO 4.63
Project fire - space and reentry vehicle static stability
REENTRY VEHICLE↗
LATERAL RANGE CONTROL BY BANKING DURING INITIAL PHASES OF SUPERCIRCULAR REENTRIES
Lateral range control by banking during initial phases of supercircular reentries
BANKING↗
STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG
Static longitudinal aerodynamics of wing and blunt body shapes for use as reentry configurations at hypersonic speed and angles of attack up to 90-deg
HYPERSONIC SPEED↗
STATIC LONGTIDUDINAL STABILITY CHARACTERISTICS OF A BLUNTED GLIDER REENTRY CONFIGURATION HAVING 79.5 DEG SWEEPBACK AND 45 DEG DIHEDRAL AT A MACH NUMBER OF 6.2 AND ANGLES OF ATTACK UP TO 20 DEG
Static longitudinal stability characteristics of blunted glider reentry configuration
LONGITUDINAL STABILITY↗
STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS AT A MACH NUMBER OF 3.11 OF SQUARE AND CIRCULAR PLAN-FORM REENTRY VEHICLES, WITH SOME EFFECTS OF CONTROLS AND LEADING-EDGE EXTENSIONS
Static stability of square and circular planform reentry vehicles at mach 3.11 - effects of controls and leading-edge extensions
STATIC STABILITY↗
AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS
Subsonic aerodynamic characteristics of delta- wing reentry vehicle with folding wingtip panels
DELTA WING↗
MODEL INVESTIGATION OF WATER LANDINGS OF A WINGED REENTRY CONFIGURATION HAVING OUTBOARD FOLDING WING PANELS
Water landings of winged reentry configuration having outboard folding wing panels - models used
WATER LANDING↗