Accession Number:

AD0862745

Title:

Evaluation of a Mariner Propellant System Bladder Using Centrifuge Facility 1-15.

Descriptive Note:

Technical rept.,

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-03-01

Pagination or Media Count:

10.0

Abstract:

Twelve evaluations of a propellant system bladder design intended for use on Mariner space vehicles were completed using the AFRPL centrifuge to impose acceleration-induced loads of ten, twenty, and thirty times the force of gravity. The AFRPL Centrifuge Facility and RPRO Operations personnel successfully produced the requested test conditions in a routine manner. Author

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE