Innovative Thermal Protection Systems (TPSs) for Trajectory Shaping Vehicles (TSVs)

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,954.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-05-M-5028
Agency Tracking Number:
F051-143-1741
Solicitation Year:
2005
Solicitation Topic Code:
AF05-143
Solicitation Number:
2005.1
Small Business Information
INTERMAT
389 Hill St., Biddeford, ME, 04005
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
834951147
Principal Investigator:
Richard McLaughlin
Senior Engineer
(207) 283-1156
rmmclaughlin@maine.rr.com
Business Contact:
David Loper
President
(207) 283-1156
intermat@gwi.net
Research Institution:
n/a
Abstract
Advanced reentry vehicles desire extended time durations in oxidizing environments, at temperatures in the range of 3000°K. State of the art nosetip materials utilize a high density carbon/carbon (C/C) composite that has a carbide center core. This attribute results in maintenance of the aerodynamic shape of the nosetip for the vehicle. Intermat has produced nosetip billets with a variety of `carbide core' configurations. These cores have been made, flush with the surface of a billet, or with the `core' submerged below the surface of the final nose tip. This technology can be applied to placing carbide material within other defined regions of a parent C/C billet such that either internal or external exposure of the carbide loaded region on the final machined nosetip surfaces. This technology could produce a nosetip with a carbide surface barrier over the shoulder and body areas of the nosetip or submerged under a layer of carbon/carbon. A "shielded" nosetip design having the outer surfaces protected by a carbide layer would permit extended flight time at high altitude, preserve shape stability of the nosetip, while providing a C/C nosetip configuration with integrated core for terminal dive.

* information listed above is at the time of submission.

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