Apollo entry aerodynamics.
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Crowder, R. S.↗
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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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Thermal control of a Mars entry capsule.
Thermal control of Mars entry capsule with fiberglass honeycomb sandwich shell analyzed with and without aft thermal curtain, emphasizing cruise-flight phase
Stultz, J. W.↗
Entry vehicles for space programs.
Earth and planetary entry vehicle designs for manned and unmanned space missions, noting thermal protection, environmental control requirements and communication systems
Greenshields, D. H.↗
Effects of environmental and ablator performance uncertainties on heat-shielding requirements for hyperbolic entry vehicles.
Environmental and ablator performance uncertainties effects on heat shielding requirements for blunt and slender hyperbolic entry vehicles
Coleman, W. D.↗
Radiofrequency transmission characteristics of candidate ablation materials for planetary-entry-vehicle heat shields
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat shields
Chapman, A. J.↗
Research problems in atmosphere entry and landing for manned planetary missions
Research problems in atmospheric entry and landing of manned planetary space flights to Mars and Venus
Syvertson, C. A.↗
Evaluation of materials in entry heating simulation
Evaluation of ablative materials in entry heating simulation
Brooks, W. A., Jr.↗
Detection of, and communication with space vehicles during atmospheric entry, problems in simulation
Detection of, and communication with spacecraft during atmospheric entry - simulation problems
Lin, S. C.↗
Guidance and navigation for entry vehicles
Guidance and navigation for atmospheric entry phase of vehicles
Source record↗
An analysis of the static and dynamic characteristics of a decoupled landing entry vehicle
Analysis of static and dynamic characteristics of entry vehicle using decoupled landing concept
Haile, J. E.↗
A terminal guidance scheme for lifting body entry vehicles
Perturbation feedback guidance for terminal phase of lifting body entry vehicle
Bryson, A. E., Jr.↗
Entry Dynamics of a Spinning Vehicle
Solution for angular motion analysis on spinning atmospheric entry vehicle
Jaffe, P.↗
Radiative energy transfer on entry into Mars and Venus Final report
Radiative energy transfer on entry into Mars and Venus
Dickerman, P. J.↗
Sensitivity guidance for entry into an uncertain Martian atmosphere
Sensitivity guidance for entry into uncertain Mars atmosphere using onboard computer
Cefola, P. J.↗
Evaluation of configuration changes on optimum structural designs for a Mars entry capsule
Optimum structural design for Martian entry capsule configurations
Cohen, G. A.↗
Trajectory control for Mars entry by discrete changes of drag surface and flight path
Discrete change in ballistic coefficient for trajectory control in Mars entry guidance
Hedge, L. F.↗
Entry aerodynamics at lunar return conditions obtained from the flight of Apollo 4 /AS-501/
Entry aerodynamics at lunar return conditions from command module of Apollo 4 flight
Hillje, E. R.↗
Effects of pressure distribution on the shape of tension shell entry vehicles
Pressure distribution effects on shape of tension shell entry vehicles determined analytically and experimentally
Sawyer, J. W.↗