Accession Number:

AD0862748

Title:

Determination of the Effects of Acceleration-Induced Loads on a Propellant System Bladder.

Descriptive Note:

Technical rept.,

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-05-01

Pagination or Media Count:

11.0

Abstract:

Four sections of propellant system bladders were evaluated during five tests on the 1-15 Test Area Centrifuge. Two specimens were accelerated to 25 g applied laterally to the test item and two specimens were accelerated to 20 g applied longitudinally. Author

Subject Categories:

  • Rocket Engines
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE