SEARCH · Search NASA
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Saturn I /SA-8/ launch vehicle and Launch Complex 37B - nitrogen and helium storage facility
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 - H- 1 rocket engine and hydraulic systems
Saturn I /SA-8/ launch vehicle and Launch Complex 37B - subsystems and components of separation and flight termination systems
Saturn I /SA-8/ launch vehicle and Launch Complex 37B - RL-10 A-3 engine and hydraulic system
Saturn I /SA-10/ launch vehicle and Launch Complex 37B - RL-10 A-3 engine and hydraulic systems
Report describes study of aerodynamic flight-control-augmentation devices proposed for use in increasing payload capabilities of future launch vehicles by allowing more aft centers of gravity. Proposed all-movable devices not only provide increased control authority during ascent trajectory, but also reduce engine gimballing requirements and enhance crew safety. Report proposes various aerodynamic control surfaces mounted fore and aft on Saturn-class launch vehicle.
Real time digital event evaluator description for Saturn launch vehicle checkout
Microcircuit development at MSFC for conversion of Saturn launch vehicle electronics
Space vehicle launching and associated noise - saturn launch vehicle - operational problems resulting from vibration
Electrical ground support equipment /EGSE/ REQUIRED by post-Saturn launch vehicle facilities and operations
Saturn I /SA-10/ - launch pad accessories functional description, finding numbers, and schematics
Computer simulation feasibility study for Saturn launch vehicle and support equipment
Description of 3 systems in which special purpose test equipment and a general purpose computer are used to test full-scale structures of the saturn launch vehicle
Stress corrosion cracking susceptibility of AM-355 stainless steel alloy for use in Saturn launch vehicles
Design of rectilinear spring-mass accelerometer for lateral control of Saturn launch vehicle
Unsteady aerodynamics studied in Saturn launch vehicle development program
Mechanical design integration of Saturn S- IVB STAGE of Saturn IB and Saturn V launch vehicle configuration