The control of motion during entry into the atmosphere
Algorithm for control of motion during entry into atmosphere
Okhotsimskiy, D. YE.↗
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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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Simulation in ground-test facilities of ablation performance of charring ablators during atmospheric entry
Ground test facility simulation of performance of charring ablators during atmospheric entry
Tompkins, S. S.↗
A parametric analysis of Venus entry heat- shield requirements
Parametric study of Venus entry heat shield weight and thickness requirements
Jaworski, W.↗
Lifting entry /L/D = or < 0.2/ for unmanned Viking class Mars landers
Lift-drag ratio for out-of-orbit and direct entry modes for unmanned Viking class Mars landers
Harrison, E. F.↗
Apollo entry summary document - Mission F /AS-505/106/LM-4/
Entry crew procedure information for use in flight planning, crew training, and preparing onboard data
Rippey, J. O.↗
Apollo entry summary document - Mission C prime
Entry crew procedures information for use in flight planning, crew training, and preparing onboard data for C prime mission
Carrico, L. D.↗
Apollo entry summary document - Mission C /SA-205, S/C-101/
Training procedures for Apollo mission C entry
Rahman, M. A.↗
Verification of entry monitor system line patterns - Project Apollo
Verification of entry monitor system line patterns for Apollo Project
Lefler, R. H.↗
Computer simulation flight acceleration facility entry monitoring system study - Project Apollo
Computer simulation and equations of motion for Apollo 8 crew training for lunar entries
Russell, W. R.↗
Excessive entry loads for abort trajectories for the nominal AS-205/101 launch profile
Excessive entry loads for abort trajectories from nominal AS-205/101 launch profile
Henderson, E. M.↗
Entry corridor definition and SM/RCS deorbit requirements for Apollo block 1 earth orbit missions. Project Apollo
Entry corridor definition and SM reaction control system for Apollo Block 1 earth orbit missions
Griffith, D. J.↗
A simulation study to evaluate backup entry ranging schemes for earth orbital missions
Hybrid computerized simulation for backup entry ranging schemes evaluation for earth orbital missions
Patterson, H. G.↗
Apollo ablator thermal performance at superorbital entry velocities
Apollo ablator thermal performance at superorbital entry velocities
Curry, D. M.↗
Heat-transfer rate and pressure measurements obtained during Apollo orbital entries
Heat transfer rate and pressure measurements obtained on Apollo command module during atmospheric entry
Lee, D. B.↗
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.↗
Atmospheric entry into Jupiter
Blunt and conical body optimum heat shield shapes for Jupiter atmospheric entry, noting shallow flight path
Tauber, M. E.↗
Tailoring polymers for entry into the atmospheres of Mars and Venus
Polymers development for ablative heat shields, aeroshell structures, antennas, insulators, electronic packaging, etc, to meet Mars and Venus atmospheric entry requirements
Nagler, R. G.↗
Role of charge separation and pressure diffusion in the gascap of entry objects
Diffusive transport term in hydrodynamic equations describing flow over strongly ablating entry objects, discussing charge separation and pressure diffusion
Howe, J. T.↗