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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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Quantum mechanical treatment of atomic center of mass motion in theory of collision effects on line shapes
The Thorad-Agena is a two-stage launch vehicle consisting of a Thorad first-stage and an Agena second-stage, connected by a booster adapter. The composite vehicle, including the shroud and the booster adapter, is about 33 meters (109 ft) long. The total weight at lift-off is approximately 91 625 kilograms (202 000 lbm).
Analysis of Saturn launch vehicle navigation, guidance, and control system
Apollo real time computer complex, remote site equipment, and communications, command, and telemetry system
Performance and orbital flight plan of SERT 2 ion thruster spacecraft
Lightning warning system of Kennedy Space Center
Calculations of rocket and air breathing propulsion system combustion chamber and nozzle flow performance
Digital computer program for aircraft configuration plotting
Automatic Mathematical Translation language software for IBM 1130
Bonding scheme of C-O in ketene described by localized orbital technique
Actoballistocardiography based on piezoelectricity for biorythmic activity, respiratory movements and heart rate of small animals
Small rocket systems research programs, discussing Apollo-Pacemaker and planetary entry parachute flight tests
Cosmic rays propagation and production in Milky Way galaxy, using equilibrium model
SERT 2 for testing ion thrustor reliability and operational characteristics, discussing design and mission objectives
Mission objectives and systems analysis of SERT 2 spacecraft
Aerobee-borne electron accelerators for ejecting electron beams into upper atmosphere
Computer programs for simulation of reconfigurable guidance and control system operation - Vol. 6