Thrust Vector Control /TVC/ system study program, volume 2 Final report
Thrust vector control system study for S-1B-5A booster - detailed report with appendices and bibliographies
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Thrust vector control system study for S-1B-5A booster - detailed report with appendices and bibliographies
Thrust vector control system study for S-1B-5A booster - summary
Fluid amplifier, servovalve, and compensation network for use with pneumatic actuator on J- 2 rocket engine Thrust Vector Control /TVC/
Electropneumatic linear actuator for thrust vector control on J- 2 rocket engine
Majority voting servoactuators for thrust vector control in Saturn S- IVB stage
Thrust vector orientation during pilot controlled lunar landing with aid of visual references
Thrust vector control orientation during pilot controlled lunar landing with aid of visual references
Thrust vector control for solid propellant rocket engines - liquid injection system, hot or cold gas systems, and gimballed nozzle systems
Optimization of hydraulic thrust vector control systems for launch vehicles - component handbook
Bending vibration equations for rocket boosted vehicle controlled by vectored thrust - structural dynamics
Vortex flow and erosion in rocket nozzles from warm-gas injection for thrust vector control
Simplified thrust vector orientation technique for establishing lunar orbits
Spacecraft guidance technique for establishing lunar parking orbits using thrust vector control in relation to lunar horizon
Compressible, inviscid secondary injection and primary flows calculated using integral relation method for blunt bodies - application to thrust vector control
Open-loop pulsed transfer functions of simplified thrust vector control system for Saturn-type vehicle with unsampled input derived by several methods
Analysis of sampled data digital compensated thrust vector control system
Determination of stability margins in channels of multiloop sampled data system, especially attitude channel of thrust vector control system
Feasibility of pneumatic digital actuator for thrust vector control