Accession Number:

AD0852845

Title:

6F Hydraulic Failure Analysis Test,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Cross, J. B.

Report Date:

1962-07-16

Pagination or Media Count:

92.0

Abstract:

The report covers results of tests conducted to investigate a sustainer hydraulic system failure which occurred at approximately booster cut-off on Missile 6F. Simulated leak tests were conducted on the sustainer hydraulic system of tail section test stand number 3, TSTS3 to assist in the flight data analysis and to determine possible causes and locations of the hydraulic failure. Author

Descriptors:

• *SURFACE TO SURFACE MISSILES
• HYDRAULIC EQUIPMENT
• LIQUID PROPELLANT ROCKET ENGINES
• BOOSTER ROCKET ENGINES
• SUSTAINER ENGINES
• LEAKAGE(FLUID)
• FAILURE
• TEST METHODS

Subject Categories:

• Hydraulic and Pneumatic Equipment
• Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE