Radiative and convective heating during atmospheric entry
Radiative and convective heating during atmospheric entry
Dirling, R. B., Jr.↗
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Results for “entry”
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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Entry length for the rocket meteorological radiation shield
Thermal entry length of temperature sensor placement in tubular radiation shield
Alsaji, S.↗
Study of direct versus orbital entry for Mars missions. Volume 7 - Supplementary report Final report
Modification to direct versus orbital entry for Mars mission as result of Mars environmental model
Craig, H. E.↗
Some problems of planetary atmosphere entry.
Space vehicles aerodynamic heating at hyperbolic entry speed, particulary ablation materials
Allen, H. J.↗
Diagnosis of planetary atmospheres from effects of entry plasma on antenna impedance.
Plasma properties and atmospheric composition deduced from antenna impedance measurements during planetary entry
Croswell, W. F.↗
A study of the effects of environmental and ablator performance uncertainties on heat shielding requirements for blunt and slender hyperbolic-entry vehicles.
Environmental and ablator performance uncertainties effects on heat shielding requirements for blunt and slender hyperbolic entry vehicles
Coleman, W. D.↗
Wind-tunnel measurements of transition on the face of a blunt entry capsule at angle of attack.
Boundary layer transition point on forward portion of blunt Apollo type entry capsule model measured in high Reynolds number wind tunnel
Jones, R. A.↗
Entry and landing requirements for manned planetary missions.
Atmospheric entry and landing requirements for manned planetary missions emphasizing problems related to Mars and Venus
Syvertson, C. A.↗
Flight simulation of night landings of lifting entry vehicles.
Lifting entry vehicles night landing flight simulation by night approaches and landings of piloted fighter aircraft with low L/D ratio
Dana, W. H.↗
Evaluation of aerothermoelasticity problems for unmanned Mars entry vehicles.
Aerothermoelasticity problems for Mars entry vehicles, discussing deceleration loads, separated hot gas flow, shield thermal gradients and oscillatory body motion
Houbolt, J. C.↗
Structural design options for planetary entry.
Structural design options for decelerative aeroshell configurations for atmospheric entry on unmanned planetary explorations
Guy, L. D.↗
Multipurpose entry vehicle requirements for unmanned landings on bodies having tenuous atmospheres.
Multipurpose entry vehicle requirements for unmanned landings on bodies in solar system having tenuous atmospheres
Harrison, E. F.↗
Entry maneuvers for large lateral and small longitudinal range.
Hypersonic entry vehicle aerodynamic maneuvers for generating large lateral and small longitudinal range
Holloway, P. F.↗
Bow shock composition and radiation intensity calculations for a ballistic entry into the Jovian atmosphere.
Bow shock temperature, pressure, composition and radiation intensity for 40 and 60 km/sec ballistic entry into Jovian atmosphere
Menard, W. A.↗
Adaptive control for Mars entry based on sensitivity analysis.
Adaptive control for Mars entry based on sensitivity analysis
Cefola, P. J.↗
Experimental aerodynamics of a rotor entry vehicle.
Aerodynamic performance tests of autorotative unpowered rotor entry vehicle model at various Mach numbers and angles of attack
Levin, A. D.↗
Summary of experimental results obtained from the NASA planetary entry parachute program.
NASA planetary entry parachute program for rocket launched and balloon deployment tests
Mcfall, J. C., Jr.↗
Drag and stability of various Mars entry configurations.
Aerodynamic drag and stability of various blunt forebody configurations for Mars entry probes from free flight test program
Krumins, M. V.↗