The object of the test was the design evaluation of the 'Moog' booster servo-cylinder under vibration and life cycling. The booster servo-cylinders tested are part of the autopilot system. They control the gimbaling of the booster rocket engines and are mounted in pairs, 90 degrees apart. (Author)
Astronautics Hydraulic Servo Cylinder 'Moog' 'D' Series, Vibration Testing and Life Testing
1959
53 pages
Report
Keine Angabe
Englisch
Hydraulic & Pneumatic Equipment , Missile Technology , Hydraulic servomechanisms , Reliability , Gyro stabilizers , Test methods , Life expectancy , Vibration , Springs , Rupture , Pressure , Fatigue(Mechanics) , Electric insulation , Electrical resistance , Fluid flow , Orifices , Transducers , Feedback , Electric currents , Moistureproofing , Surface to surface missiles , Atlas , Closed loop systems , Control , Control systems , Xsm-65d missiles
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