The degradation of the pulsed performance of low-thrust, cold-gas, jet reaction systems is shown; also, the experimental data are compared with analytical results. Preliminary experimental results using anhydrous ammonia gas as a propellant are included. The experimentation conducted on a single-axis attitude control system utilizing a fluid flywheel is presented, along with an analysis of this system. The preliminary results of an analysis of the singleaxis vehicle simulator incremental follow-up servo are given. In addition, a specific impulse pneumatic test facility and a manned tracking target symbol generator are described. (Author)
Electonics Research Program. Satellite Attitude Control System Experiments
1964
84 pages
Report
No indication
English
Manned Spacecraft , Navigation, Guidance, & Control , Attitude control systems , Control jets , Flywheels , Satellites (Artificial) , Satellite attitude , Fluids , Specific impulse , Ammonia , Horizon scanners , Simulation , Analog computers , Spheres , Gas bearings , Reaction wheels , Fluid flywheels
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