Determination of the Effects of Acceleration-Induced Loads on a Propellant System Bladder.
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
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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
- Rocket Engines
- Ground Support Systems and Facilities for Space Vehicles