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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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Load relief autopilot to minimize launch vehicle thrust vector deflection angle required for vehicle stability during flight through design winds
Analog and digital simulation of performance prediction for test assembly on turbine pump self-compensating thrust balance systems
Coaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engine
Performance of vortex valve controlled secondary injection thrust vector system for solid propellant rocket motor control
Reliability analyses and failure probabilities of S-4B stage automatic pilots and hydraulic thrust vector control system configurations, and compatibility with actuator
Trajectory optimization problems in mechanics of low thrust propulsion for solar sail and power limited space flights
Electrode misalignments effects on thrust vector control for Kaufman electric rocket thrustors, noting implications for SERT 2 mission
Solar electric low thrust propulsion application to Jupiter swingby mission to outer planets
Ionized plasma electromagnetic accelerators, noting thrust efficiency variation due to difference between supplied and expelled mass flow rate
Manual thrust vector control development for Apollo Command and Service Module Stabilization and Control System
Approximate analytic solution for variables describing three dimensional solar powered heliocentric low thrust trajectory in vicinity of ecliptic plane
Motion equations of spin stabilized rocket under thrust with jet damping, variable mass and momentum effects and all angular disturbances
Low thrust solid and hybrid propulsion systems requirements for future missions including ATS-4, Voyager, Apollo Telescope Mount and manned interplanetary vehicle
Solar electric thrust system technology concerning performance, thruster control system stability and method for solution
Constant thrust electric propulsion systems performance with coast trajectories presented for 1.0 AU extraecliptic missions
MIRA 150A variable thrust rocket engine applied to manned lunar exploration flying systems
Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
Solar electric low thrust propulsion application to Jupiter swingby mission to outer planets