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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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Determination of optimum 3-dimensional trajectories to inject a saturn c-5 rocket into a space-fixed circular orbit
Description of saturn v checkout facilities at the merritt island launch area
Obtention of a launch window, as a function of allowable performance loss, for placing a saturn v in a circular orbit in a prespecified space-fixed plane
Launch facility complex for the saturn c-5 rocket which will carry apollo spacecraft to the moon
Design, development, fabrication, and preflight certification testing of Saturn V S-1C pressure switches
Saturn V instrument unit including structural, environmental control and guidance and control systems
Saturn V space station system selection and choice of orbit, crew and logistic support
Saturn V launch control and checkout system discussing interconnected computer complexes, digital and video displays and programming methods
Saturn V mechanical ground support equipment including umbilical, disconnector, pneumatic, servicing, handling and auxiliary systems
Gas-tungsten arc welding for positioning and inside-locking of liquid oxygen /LOX/ tunnel of Saturn V booster
Saturn V S-IC stage engine guidance, flight control and gimbal servoactuation system for Apollo spacecraft
Test program limited to Saturn V nuclear stage requirements, assessing performance of saturated gaseous hydrogen as monopropellant in conical nozzles
Onboard checkout functions for Saturn V instrument unit and S-IVB stages
Interaction of structure and liquid of the Saturn V sound suppressor system
Space missions using electric propulsion systems launched by Saturn V or larger boosters - use of chemical and nuclear rockets
Computer weight/performance prediction method to assess design and program and to optimize structural systems similar to those of Saturn V for management planning
Head to head tests on Saturn V hydrodynamic support to determine performance compared with mathematical model prediction
Reliability analysis for Saturn V hydrodynamic support equipment