Hypersonic nonequilibrium flow at re-entry of space vehicles and its thermodynamic relations
Hypersonic nonequilibrium flow at reentry of space vehicles and thermodynamic relations
THERMODYNAMIC PROPERTY↗
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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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The Effects of Atmospheric Re-entry on Graphitic Particles
Effects of atmospheric reentry on graphite particles
GRAPHITE↗
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↗
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↗
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
ENVIRONMENT SIMULATION↗
Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.
Symmetrical equilibrium flow past blunt body at superorbital reentry conditions calculated by integrating motion equations across shock layer
FLOW STABILITY↗
Free-flight measurements of aerodynamic viscous effects on lifting re-entry bodies.
Lift-drag ratio, lift and drag coefficients and angle of attack effects on Gemini and Apollo reentry vehicles measured in shock tunnel under free flight conditions
VISCOUS DRAG↗
Magnetogasdynamic re-entry phenomena.
MGD reentry flow regimes analyzed, noting increased bow shock standoff distance and drag, comparing in-flight and laboratory simulation
MAGNETOGASDYNAMICS↗
Error analysis of hybrid simulation for spacecraft re-entry studies Final report
Error analysis of hybrid simulation for six degree of freedom equations of motion for spacecraft reentry
Jackson, A. S.↗
Application of multivariable search techniques to the shaping of minimum total heat re-entry bodies at hyberbolic velocity
Heat minimization and optimal shapes for bodies of revolution entering earth atmosphere at hyperbolic speeds
Hague, D. S.↗
Space and re-entry systems - Development of advanced soil sampler technology, volume 2 Final report, 28 Jun. 1967 - 31 Jan. 1968
Advanced soil sampler technology
Bachle, W. H.↗
Space and re-entry systems - Development of advanced soil sampler technology, volume 1 Final report, 28 Jun. 1967 - 31 Jan. 1968
Development, and evaluation of sieve sampler, and rotating wire brush sampler for planetary soil probing
Bachle, W. H.↗
Dynamic stability of space vehicles. Volume 12 - Re-entry vehicle landing ability and control
Control and stability aspects prior to spacecraft landing, and propulsive assist to landing spacecraft
Kuchta, B. J.↗
Effect of re-entry vehicle environment on electromagnetic radiation.
RF/plasma interactions relative to reentry plasma diagnostics and microwave transmission, noting increased hot air susceptibility to RF breakdown
Chown, J. B.↗
Exploratory investigations of the effects of gas injection through a porous model on separation, transition, static stability and control effectiveness of a blunt re-entry body at Mach number 7.3.
Nitrogen injection on blunt reentry body, investigating influence on separation, transition, static stability and control effectiveness
Donohoe, J. C.↗
A neighboring optimum feedback control scheme based on estimated time-to-go with application to re-entry flight paths.
Neighboring optimum feedback control scheme based on estimated time-to-go applied to reentry flight paths
Bryson, A. E., Jr.↗
Simulation of the Apollo Command Module aerodynamics at re-entry altitudes.
Apollo Command Module aerodynamics at reentry altitudes simulated by models in hypersonic flow
Boylan, D. E.↗