Composite material compatibility with liquid and gaseous oxygen-Reference-Cited by-同舟云学术

Composite material compatibility with liquid and gaseous oxygen

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA Applied Aerodynamics Conference
language:
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Author:

Robinson Michael¹,Stolzfus Joel²,Owens Thomas³

Affiliation:

1. Boeing Co., Space and Communications Group, Huntington Beach, CA

2. NASA, White Sands Test Facility, Las Cruces, NM

3. NASA, Marshall Space Flight Center, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1215

Reference23 articles.

1. Maximum-Rate Theory of Impact Sensitivity

2. NASA-MSFC Specification 106B (MSFCSPEC-106B), "Testing Compatibility of Materials for Liquid Oxygen Systems, October 6, 1967.

3. Blackstone, W.R.and Ku,P.M."An Assessment of Impact Test Techniques for Determining the Fire or ExplosionHazards of MaterialsExposedtoLiquidOxygen",MaterialsResearch andStandards,June, 1971.

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