Accession Number:

AD0842100

Title:

4C AND 11D FAILURE ANALYSIS OF HELIUM PRESSURE REGULATOR (FUEL TANK) DWR. NO. 27-08217-3,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1960-08-11

Pagination or Media Count:

19.0

Abstract:

This test was conducted to analyze failures that occurred in the airborne pressurization system of missiles 4C and 11D. The objective of the test was to determine if heating of the motor section pressurebleed line on the regulator would result in a condition similar to that which caused the failures. Author

Subject Categories:

  • Test Facilities, Equipment and Methods
  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE