The decline and fall of IMP 3 - Second report
Reentry predictions for Explorer 28 satellite
Lowrey, B. E.↗
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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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An analytical investigation of the aerodynamic and performance characteristics of an unpowered rotor entry vehicle
Aerodynamic and performance characteristics of unpowered rotor reentry vehicle
Levin, A. D.↗
Prediction of heat transfer in multiple glaze transparencies Final report
Techniques for evaluating thermal behavior of window systems for space vehicles exposed to environmental conditions attendant to planetary reentry
Source record↗
Planning research in the area of launch vehicle and propulsion programs Progress report, 1-31 Mar. 1968
Program and report reviews on launch vehicle upper stages and propulsion of advanced reentry spacecraft
Davis, B. W.↗
Biosatellite 2 experiment environment
Reentry vehicle and experiment packages of Biosatellite 2 spacecraft
Look, B. C.↗
A study of the effects of environmental and ablator performance uncertainties on heat shielding requirements for hyperbolic entry vehicles, volume 1
Environmental and ablative materials performance affecting heat shielding requirements of slender and blunt vehicles during hyperbolic reentry
Chin, J. H.↗
Aerodynamic characteristics of a modified cone - Conical-frustum entry configuration at Mach 6.0
Aerodynamic characteristics of modified conical lifting reentry vehicle at hypersonic speeds
Ashby, G. C., Jr.↗
A study of the effects of environmental and ablator performance uncertainties on heat shielding requirements for hyperbolic entry vehicles. Volume 2 - Summary of calculations
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry vehicles
Chin, J. H.↗
The effects of shock layer radiation and viscous coupling on the total heating rate to a reentering blunt body
Coupling radiative and convective heat transfer in hypersonic blunt body reentry
Engel, C. D.↗
Body rotation effects on melting ablation
Rotation effects on melting ablation on reentry of axisymmetric bodies
Cochran, T. H.↗
Impedance of plasma coated axial slot antenna
Plasma sheath effect on reentry communication system with slot antennas
Campbell, T. G.↗
Feasibility tests of a radioisotope type ablation measuring system
Reentry shielding ablation measured by imbedded radioactive isotopes with radiation dector
Le Bel, P. J.↗
Transition and flow reattachment behind an Apollo-like body at Mach numbers to 9
Transition from laminar to turbulent flow in near wake of supersonic reentry body
Kruse, R. L.↗
Luminous efficiencies of three nickel artificial meteors between 9.8 and 11.4 kilometers per second
Luminous intensity and efficiency parameters for hypersonic reentry of nickel artificial meteors
Bess, T. D.↗
A Technique for Determining the Spatial Distribution of Relative Radiant Intensity in Shock Layers over Bodies at Angle of Attack at Hyersonic Velocities
Spatial distribution of radiant heat in reentry vehicle hypersonic shock layers at angle of attack
Reynolds, R. M.↗
Heat shield instrumentation - Development and evaluation
Methods and techniques for monitoring critical heat shield parameters during spacecraft reentry
Hicks, E. W., Jr.↗
Newtonian aerodynamics for general surfaces.
Newtonian flow model, calculating hypersonic reentry aerodynamic forces for complicated body shapes
Heybey, W. H.↗
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.↗