ASTRONAUTICS HYDRAULIC SERVO CYLINDER 'MOOG' 'D' SERIES, VIBRATION TESTING AND LIFE TESTING,

reportActive / Technical Report | Accession Number: AD0832295 | Need Help?

Abstract:

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

Author(s):
Soltmann, J. D.
Author Organization(s):
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
Pagination:
0053

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
GDA-7A-2115
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
Weapons Technologies
Descriptor(s):
*HYDRAULIC SERVOMECHANISMS, RELIABILITY, GYRO STABILIZERS, TEST METHODS, LIFE EXPECTANCY(SERVICE LIFE), VIBRATION, SPRINGS, RUPTURE, PRESSURE, FATIGUE(MECHANICS), ELECTRICAL INSULATION, ELECTRICAL RESISTANCE, FLUID FLOW, ORIFICES, TRANSDUCERS, FEEDBACK, ELECTRIC CURRENT, MOISTUREPROOFING, SURFACE TO SURFACE MISSILES
Field(s)/Group(s):
Hydraulic and Pneumatic Equipment, Surface-Launched Guided Missiles
Keyword(s):
ATLAS, CLOSED LOOP SYSTEMS, CONTROL, CONTROL SYSTEMS, XSM 65D MISSILES
Report Date:
1959 May 27