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Methods for Decontamination of a Bipropellant Propulsion SystemMost propulsion systems are designed to be filled and flown, draining can be done but decontamination may be difficult. Transport of these systems may be difficult as well because flight weight vessels are not designed around DOT or UN shipping requirements. Repairs, failure analysis work or post firing inspections may be difficult or impossible to perform due to the hazards of residual propellants being present.
Document ID
20120007434
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
McClure, Mark B.
(NASA Johnson Space Center Houston, TX, United States)
Greene, Benjamin
(Jacobs Technology, Inc. Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
April 30, 2012
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
JSC-CN-26208
Report Number: JSC-CN-26208
Meeting Information
Meeting: 41st Structures and Mechanical Behavior Subcommittee
Location: San Antonio, TX
Country: United States
Start Date: April 30, 2012
End Date: May 4, 2012
Sponsors: Johns Hopkins Univ.
Distribution Limits
Public
Copyright
Public Use Permitted.
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