Mars entry and landing capsule.
Mars planetary entry and landing model tests, demonstrating technological feasibility of mission
Casani, E. K.↗
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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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Ablative heat shields for planetary entry vehicles.
Ablative heat shield materials for Mars and Venus atmospheric entries
Sparhawk, H. E.↗
Downstream radiation flux to blunt entry vehicles.
Downstream radiation flux distribution calculated for blunt entry bodies, considering self absorption effects
Burns, R. K.↗
Status of the aerodynamic characteristics of the Apollo entry configuration.
Entry phase flight data of Missions AS-202, Apollo 4 and 6 compared with wind tunnel aerodynamics data
Hillje, E. R.↗
Atmospheric entry into the major planets with emphasis on Jupiter.
Blunt and conical body optimum heat shield shapes for Jupiter atmospheric entry, noting shallow flight path
Tauber, M. E.↗
Aeroshell structural development for Martian entry.
Aeroshell structural development for Mars flyby and entry landing mission compatible with Atlas/Centaur launch vehicle
Garba, J. A.↗
Simulation of Venus atmospheric entry by earth reentry.
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry
Spiegel, J. M.↗
Structural and decelerator design options for Mars entry.
Structural design options for decelerative aeroshell configurations for atmospheric entry on unmanned planetary explorations
Guy, L. D.↗
Angle-of-attack motion of a spinning entry vehicle.
Angle of attack effect on motion throughout entry of spinning descending vehicle, noting effects of transverse angular velocity and spin rate
Jaffe, P.↗
Thermal entry for low Reynolds number turbulent flow.
Thermal entry problem solution for low Reynolds number turbulent gas flow based on Reynolds number dependent velocity profile
Mceligot, D. M.↗
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.↗
Entry flight research and experimentation.
Configuration, trajectory planning, instrumentation, calorimetry and aerodynamic heating for planetary atmosphere entry
Stone, D. G.↗
Guidance and control for atmospheric entry.
Guidance and control concepts and hardware for atmospheric entry of Mercury, Gemini and Apollo spacecraft
Duncan, R. C.↗
Entry research and development program management.
Program definition and government-industry relationships in entry research and development program management
Shea, J. F.↗
Apollo entry aerodynamics.
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Crowder, R. S.↗
Thermal entry for low Reynolds number turbulent flow.
Thermal entry problem solution for low Reynolds number turbulent gas flow based on Reynolds number dependent velocity profile
Mceligot, D. M.↗
Proton entry into the magnetosphere on May 26, 1967.
Low energy solar protons entry into magnetosphere on 26 May 1967 showing diffusion control
Bostrom, C. O.↗
Planetary entry body heating rate measurements in air and Venus atmospheric gas up to T equal 15,000 deg K.
Convective plus radiative shock tube model stagnation point heating rate measurements for planetary entry heating rate in air and Venus gas
Livingston, F.↗