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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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Mechanical impact attenuation system for Apollo spacecraft provides stable land landing platform, noting deployed heat shields, extended legs, pneumatic bags, etc
Promethium isotope heated ammonia microthrustor using heat shield package to maintain temperature
Hypervelocity heat protection, surface heat shielding, and internal temperature rise of Teflon, phenolic nylon, epoxy resin in glass honeycomb, and silicone elastomer
Nucleonic measurement of ablative heat shield material recession
Movement of forward heat shield in Apollo command module turbulent reverse flow wake
Aeroheating and aeroshell configuration analyses, and ablative heat shield design criteria - direct versus orbital entry for Mars missions
Convective and radiative heat transfer to reentry vehicles protected by ablation heat shields
Space to reentry environmental sequence simulator for heat shield materials uninterrupted vacuum transfer without exposure to atmosphere
Semiempirical correlation techniques for predicting charring ablation performance of Apollo heat shield in turbulent flow
FORTRAN 4 program for predicting charring ablation performance of Apollo heat shield in turbulent flow
Pyrotechnic-activated heat-shield ejection system for NASA Project Fire
Buoyant Venus station mission study for 1972 - 1973 launch period - backup data including atmospheric models, heat shield requirements, etc.
Investigation of low density ablative materials for heat shields on reentry vehicles
Effect of heat shield flexibility on water landing loads of Apollo spacecraft models
Ablation behavior of heat shield of Apollo command module over wide range of thermal environments
Heat flux sensor assembly with proviso for heat shield to reduce radiative transfer between sensor elements
Blunt and conical body optimum heat shield shapes for Jupiter atmospheric entry, noting shallow flight path
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry