Study of thermal protection requirements for a lifting body entry vehicle suitable for near-earth missions Final report
Reentry and abort trajectory analyses, and thermal protection requirements for lifting body entry vehicles
THERMAL PROTECTION↗
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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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Study of thermal protection requirements for a lifting body entry vehicle suitable for near-earth missions Summary report
Weight estimates of thermal protection systems for lifting body reentry vehicle suitable for near earth missions
LIFTING BODY↗
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↗
Infrared acquisition and tracking system - Preliminary mission system specifications
Specifications for infrared acquisition and tracking system used for aircraft monitoring of Apollo command module reentry
COMMAND MODULE↗
Development of an electron density probe Final report, 28 May 1965 - 28 Feb. 1966
Electron density probe and its application in separated flow region of reentry Apollo spacecraft for typical trajectory
ELECTRON DENSITY↗
Optimum navigation measurements
Optimum navigation measurements for satellite orbit and hyperbolic free fall reentry
HYPERBOLIC REENTRY↗
Feasibility, parametric design, and comparative analysis of an unguided solid fuel rocket vehicle with solar orbit, earth probe, and re-entry mission capabilities
Feasibility, parametric design, and comparative analysis of unguided solid fuel rocket vehicle with solar orbit, earth probe, and reentry mission capabilities
STRUCTURAL DESIGN↗
Evaluation of lateral-directional handling qualities of piloted re-entry vehicles utilizing fixed-base and in-flight evaluations
Lateral directional handling qualities of piloted reentry vehicles utilizing fixed base and in flight evaluations
T-33 AIRCRAFT↗
Effects of two probe antennas on aerodynamic characteristics of Apollo spacecraft at Mach 10.03
Effects of two interchangeable probe antennas on aerodynamic characteristics of Apollo reentry vehicle model at Mach number 10.03
ANTENNA↗
Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods
Afterbody heating by Mercury spacecraft during reentry determined from skin temperatures
MERCURY CAPSULE↗
Heat-transfer measurements on the rotor blade of a rotor entry vehicle model
Heat transfer measurements on rotor blade of reentry vehicle model
ROTOR BLADE↗
A neighboring optimum feedback control scheme based on estimated time-to-go with application to re-entry flight paths
Neighboring optimum feedback control system for reentry flight paths
FLIGHT PATH↗
Aerodynamic effects of bulbous bases
Separated flow effect on dynamic behavior of bulbous-based reentry vehicles
REENTRY VEHICLE↗
Aerodynamic investigation of some high-drag entry shapes at Mach 15.4
Effects of body shape, nose radius, and shoulder shape of reentry body on aerodynamic drag
DRAG COEFFICIENT↗
Collet release mechanism
Release mechanism for separating and ejecting reentry vehicle payload from booster
SEPARATION↗
Analytical, experimental, and developmental work for a radiative heating system, volume I Final report
Optical system for radiative heat transfer for thermal protection of reentry vehicle
THERMAL PROTECTION↗
Stability derivatives by rheoelectric analog.
Slender body theory application in obtaining aerodynamic stability derivatives for reentry vehicles via electrical analogy
SLENDER BODY↗
Equilibrium air radiation from shock layers at 11.3 km/sec.
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
HIGH TEMPERATURE AIR↗