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) : Denker, John

Report Date : MAY 1969

Pagination or Media Count : 11

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)

Descriptors :   (*LAUNCH VEHICLES, PROPELLANT TANKS), (*PROPELLANT TANKS, PROPELLANT CONTROL), LIQUID ROCKET PROPELLANTS, EVACUATION, SPACE ENVIRONMENTS, AERODYNAMIC LOADING, CENTRIFUGES, TEST METHODS.

Subject Categories : Rocket Engines
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE