Accession Number:

AD0861426

Title:

Tube Connector Development

Descriptive Note:

Final technical rept. Sep 1964-Dec 1968

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDSAFB CA

Personal Author(s):

Report Date:

1969-07-01

Pagination or Media Count:

101.0

Abstract:

During the development of rocket propulsion systems, separable connectors were needed that could effectively perform in rocket-system environments. A connector was designed and designated as the AFRPL connector. Qualification tests were conducted to verify that the AFRPL connector could meet the extreme requirements of rocket fluid systems. The report is concerned with the testing phase of the program.

Subject Categories:

  • Pumps, Filters, Pipes, Tubing, Fittings and Valves
  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE