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Development of Segmented Composite Toroidal TanksThe conservation of weight and space are major challenges for launch vehicles, especially upper stages. Upper-stage launch vehicles are confined by the space of the payload fairing of the first stage and it is difficult to stack fuel and oxidizer tanks end-to-end. Toroidal tanks have been studied as a way to help solve this problem. A toroidal tank concept would allow a portion of another tank, or part of an engine, to pass through its center opening. A toroidal tank assembly would be especially beneficial if it could somehow handle structural loads of the vehicle. Marshall Space Flight Center, along with ATK Thiokol Propulsion, is designing and fabricating a toroidal tank composed of individual conformal segments. Each conformal segment will be a metal-lined composite over-wrapped vessel. This paper will demonstrate unique materials and processing approaches that are overcoming hurdles for the fabrication of this vessel.
Document ID
20030001001
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
DeLay, Thomas K.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Roberts, J. Keith
(Thiokol Propulsion Brigham City, UT United States)
Munafo, Paul M.
Date Acquired
August 21, 2013
Publication Date
January 1, 2002
Subject Category
Launch Vehicles And Launch Operations
Meeting Information
Meeting: AMPET
Location: Huntsville, AL
Country: United States
Start Date: September 16, 2002
End Date: September 18, 2002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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