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Materials Compatibility Testing in Concentrated Hydrogen PeroxideMaterials test methods from the 1960's have been used as a starting point in evaluating materials for today's space launch vehicles. These established test methods have been modified to incorporate today's analytical laboratory equipment. The Orbital test objective was to test a wide range of materials to incorporate the revolution in polymer and composite materials that has occurred since the 1960's. Testing is accomplished in 3 stages from rough screening to detailed analytical tests. Several interesting test observations have been made during this testing and are included in the paper. A summary of the set-up, test and evaluation of long-term storage sub-scale tanks is also included. This sub-scale tank test lasted for a 7-month duration prior to being stopped due to a polar boss material breakdown. Chemical evaluations of the hydrogen peroxide and residue left on the polar boss surface identify the material breakdown quite clearly. The paper concludes with recommendations for future testing and a specific effort underway within the industry to standardize the test methods used in evaluating materials.
Document ID
20000091531
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Boxwell, R.
(Orbital Sciences Corp. Chandler, AZ United States)
Bromley, G.
(Orbital Sciences Corp. Chandler, AZ United States)
Mason, D.
(Orbital Sciences Corp. Chandler, AZ United States)
Crockett, D.
(Orbital Sciences Corp. Chandler, AZ United States)
Martinez, L.
(Orbital Sciences Corp. Chandler, AZ United States)
McNeal, C.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Lyles, G.
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Inorganic, Organic And Physical Chemistry
Meeting Information
Meeting: Joint Propulsion
Location: Huntsville, AL
Country: United States
Start Date: July 17, 2000
End Date: July 19, 2000
Sponsors: Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NCC8-98040
Distribution Limits
Public
Copyright
Public Use Permitted.
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