Evaluation of a Mariner Propellant System Bladder Using Centrifuge Facility 1-15.
AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA
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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
- Rocket Engines
- Ground Support Systems and Facilities for Space Vehicles