Apollo Saturn Heat Shield in Orbit Test
Apollo/Saturn I unmanned space flight to test command module ablative heat shield
APOLLO PROJECT↗
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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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Apollo infrared acquisition and tracking system Summary report
Airborne infrared detection, acquisition, and tracking system for Apollo command module reentry
TRACKING SYSTEM↗
Man-in-space communications subsystem.
Communications subsystem providing S-band link between LEM and Earth and VHF link between LEM AND Command Module
SPACE COMMUNICATION↗
Cassegrainian monopulse tracking antenna for space rendezvous.
Cassegrain monopulse tracking antenna for LEM and Command Module rendezvous guidance
APOLLO PROJECT↗
Analytical technique characterizes all trace contaminants in water
Properly programmed combination of advanced chemical and physical analytical techniques characterize critically all trace contaminants in both the potable and waste water from the Apollo Command Module. This methodology can also be applied to the investigation of the source of water pollution.
Foster, J. N.↗
Study of Apollo water impact Final report
Computer program for determining hydroelastic response of command module during impact into water
Wilkinson, J. P. D.↗
Study of Apollo water impact. Volume 11 - User's manual for unsymmetric shell of revolution analysis Final report
Users manual on static and dynamic computer programs on linear elastic thin shell theory - Apollo command module water impact
Carrion, E.↗
Study of Elastomeric Shield Materials /ESM/ for Apollo
Flight test and evaluative data relating to design and use of elastomeric shield materials for thermal shield for Apollo command module
Source record↗
Water pressure and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation system
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module with deployed heat shield impact attenuation system
Stubbs, S. M.↗
Study of Apollo water impact. Volume 1 - Hydrodynamic analysis of Apollo water impact Final report
Mathematical model for Apollo command module impact analysis on water
Li, T.↗
A study of ignition pressure spiking in attitude control engines. Volume 1 - Evaluation of the use of catalytic surfaces to eliminate ignition pressure spiking Final report, 1 Jul. 1966 - 30 Apr. 1967
Effects of injector catalytic surfaces on ignition pressure spiking in Apollo command module engine
Falkenstein, G. L.↗
RTCC requirements for mission G - Landing site determination using onboard observations, part 2 Final report
Computer programs for evaluation of telemetered rendezvous radar tracking data of orbiting command module and lunar module landing site determination
Austin, G. A.↗
A quasi-steady state analysis of the dynamic behavior of a conic body moving in a nonuniform wake
Movement of forward heat shield in Apollo command module turbulent reverse flow wake
De Fife, J.↗
Transient thermal simulation of Apollo spacecraft and ECS.
Apollo spacecraft command module analytical thermal model, discussing correlation of model with test data
Frahm, J. R.↗
A parametric analysis of three vehicle shapes for use as hyperbolic entry.
Apollo command module, biconic and cone hyperbolic reentry vehicles engineering, discussing L/D ratio, heat protection and weight
Anderson, J. L.↗
Apollo reaction control systems.
Apollo reaction control systems, describing command module, service module, lunar module, engine qualifications, etc
Vaughan, C. A.↗
Apollo entry aerodynamics.
Apollo spacecraft command module aerodynamic characteristics during entry compared with wind tunnel test predictions
Crowder, R. S.↗
An Investigation of Ablation Behavior of Avcoat 5026-39/M over a Wide Range of Thermal Environments
Ablation behavior of heat shield of Apollo command module over wide range of thermal environments
Crouch, R. K.↗