Accession Number:

AD0843372

Title:

Pressure Transients in Missile Hydraulic System During Rise-Off,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Martin, R. I.

Report Date:

1961-11-16

Pagination or Media Count:

23.0

Abstract:

The objectives of the test was to investigate and determine the cause of pressure transients in the missile hydraulic system. Author

Descriptors:

• *HYDRAULIC EQUIPMENT
• TRANSIENTS
• SUSTAINER ENGINES
• FAILURE
• LAUNCHING
• PRESSURE
• HYDRAULIC PRESSURE PUMPS
• TRANSDUCERS
• GROUND SUPPORT EQUIPMENT
• VERNIER ROCKET ENGINES
• BOOSTER ROCKET ENGINES
• CAPTIVE TESTS
• GUIDED MISSILES

Subject Categories:

• Hydraulic and Pneumatic Equipment
• Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE