NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
SLM Produced Hermetically Sealed Isolation ValveMarshall Space Flight Center (MSFC) has developed a valve concept to replace traditional pyrotechnic-driven isolation valves. This paper will describe the valve design and development process. The valve design uses a stem/wedge to support a disk inside the valve. That disk hermetically seals the pressurized fluids. A release mechanism holds the stem/wedge and a large spring in place. When required to open, a solenoid is energized and pulls the release mechanism allowing the spring to pull the stem/wedge away from the disk. Now the disk is unsupported and the pressure ruptures the disk allowing flow to the outlet of the valve. This paper will provide details of this design, describe the development testing, and show the results from the valve level tests performed. Also, a trade study is presented to show the advantages of this design to a conventional pyrotechnic-based valve.
Document ID
20150004081
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Richard, James
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
April 2, 2015
Publication Date
May 1, 2014
Publication Information
Publication: The 42nd Aerospace Mechanism Symposium
Subject Category
Spacecraft Design, Testing And Performance
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available