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