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Innovative Method for Developing a Helium Pressurant Tank Suitable for the Upper Stage Flight ExperimentThe AFRL USFE project is an experimental test bed for new propulsion technologies. It will utilize ambient temperature fuel and oxidizers (Kerosene and Hydrogen peroxide). The system is pressure fed, not pump fed, and will utilize a helium pressurant tank to drive the system. Mr. DeLay has developed a method for cost effectively producing a unique, large pressurant tank that is not commercially available. The pressure vessel is a layered composite structure with an electroformed metallic permeation barrier. The design/process is scalable and easily adaptable to different configurations with minimal cost in tooling development 1/3 scale tanks have already been fabricated and are scheduled for testing. The full-scale pressure vessel (50" diameter) design will be refined based on the performance of the sub-scale tank. The pressure vessels have been designed to operate at 6,000 psi. a PV/W of 1.92 million is anticipated.
Document ID
20010046957
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
DeLay, Tom K.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Munafo, Paul
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Subject Category
Engineering (General)
Meeting Information
Meeting: AIAA Conference
Location: Albuquerque, NM
Country: United States
Start Date: August 28, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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