High Temperature Structures With Inherent Protection

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$70,000.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
NNL05AB00P
Award Id:
76849
Agency Tracking Number:
040659
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
7960 S. Kolb Rd., Tucson, AZ, 85706
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
147518286
Principal Investigator:
JamesWithers
Principal Investigator
(520) 574-1980
jcwithers@mercorp.com
Business Contact:
JamesWithers
Chief Executive Officer
(520) 574-1980
jcwithers@mercorp.com
Research Institute:
n/a
Abstract
The hot structures for current space vehicles require an atmospheric entry thermal protection system. Reusable hot structures that can function without requiring any atmospheric entry thermal protection system for space vehicle would constitute a paradigm. A high temperature stable fiber reinforcement and a ceramic material that exhibits atmospheric entry thermal stability can be combined into a composite which possess the mechanical properties to serve as a reusable hot structure that can function without any atmospheric entry thermal protection system. This unique and new ceramic matrix composite (CMC) will be developed and characterized to demonstrate it can meet the requirements of a reusable hot structure for space vehicles which can operate without any atmospheric entry thermal protection system and optimized samples will be delivered for more detailed testing at NASA

* information listed above is at the time of submission.

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