Flash data and reentry trajectory system
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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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Navigational device, invented to aid recovery of spacecraft from any orbit, also illustrates motions of satellites relative to earth and their entry-ranging requirements. Device rapidly and accurately defines lateral range requirements for spacecraft returning to any desired site without manual or computerized calculation of orbital equations of motion.
Two stage to orbit reusable spacecraft system for use in transporting cargo and passengers to and from earth orbital space stations
Program plans for design, manufacturing, development test, launch operations, and vehicle recovery
Aerodynamic and thermodynamic performance of reusable two stage system
Rocket engine criteria for reusable space transport system - Vol. 3, Part A
Ablative heat shield char layer, examining reacting nonequilibrium pyrolysis gas flow
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