Accession Number:

AD0832295

Title:

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

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Soltmann, J. D.

Report Date:

1959-05-27

Pagination or Media Count:

53.0

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

Descriptors:

• *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

Subject Categories:

• Hydraulic and Pneumatic Equipment
• Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE