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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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Pneumatic system for distributing nitrogen and helium to Saturn I /SA-10/ launch vehicle
Inflight stage separation and flight termination system for Saturn I /SA-10/ launch vehicle
Nitrogen and helium storage facility for Launch Complex 37B of Saturn I /SA-10/ launch vehicle
Saturn I /SA-10/ launch vehicle mechanical flight summary
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - legend and composite schematic
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - liquid hydrogen fuel system
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - H- 1 rocket engine and hydraulic systems
Saturn I /SA-10/ launch vehicle and Launch Complex 37B functional systems description - environmental conditioning, index of finding numbers, and mechanical schematics
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - RL-10 A-3 engine and hydraulic systems
Saturn 8, 9, and 10 launch vehicles - dispersions and application to nominal trajectory, mission objectives, root sum square method, and engine- out capability
Saturn SA-10 range safety data, and reliability analysis of S-IV-8 and S-IV-10 stages
Saturn I /SA-10/ - launch pad accessories functional description, finding numbers, and schematics
Vibration and acoustic analysis Saturn SA-10 FLIGHT