Advanced Crew Escape Suits (ACES) : Particle Impact Test
- Author:
- Stoltzfus, Joel M.
- Published:
- [2009].
- Physical Description:
- 1 electronic document
- Additional Creators:
- Rosales, Keisa R.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary:
- NASA Johnson Space Center (JSC) requested NASA JSC White Sands Test Facility to assist in determining the effects of impaired anodization on aluminum parts in advanced crew escape suits (ACES). Initial investigation indicated poor anodization could lead to an increased risk of particle impact ignition, and a lack of data was prevalent for particle impact of bare (unanodized) aluminum; therefore, particle impact tests were performed. A total of 179 subsonic and 60 supersonic tests were performed with no ignition of the aluminum targets. Based on the resulting test data, WSTF found no increased particle impact hazard was present in the ACES equipment.
- Other Subject(s):
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 20080048305.
12th International Symposium on Flammabililty and Sensitivity of Materials in Oxygen-Enriched Atmospheres; 7-9 Oct. 2009; Berlin; Germany. - Terms of Use and Reproduction:
- No Copyright.
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