Accession Number:

AD0832295

Title:

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

Personal Author(s):

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1959-05-27

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

Pages:

0053

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File Size:

0.00MB

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