Lightweight, Low Thermal Conductivity Thermal Protection System for Military Space Plane

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,986.00
Award Year:
1998
Program:
SBIR
Phase:
Phase I
Contract:
n/a
Award Id:
41003
Agency Tracking Number:
41003
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
12173 Montague St, Pacoima, CA, 91331
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Jerry W. Brockmeyer
(818) 899-0236
Business Contact:
() -
Research Institute:
n/a
Abstract
The temperature constraints of current thermal protection system (TPS) materials limit the flight path and thus the mission flexibility of existing and new hypersonic and spacecraft reentry vehicles, such as the Military Space Plane (MSP). Lightweight materials with increased TPS operational temperature to over 3000 degreeF and improved surface durability and erosion resistance will create numerous opportunities for these applications. The shortcomings of current insulating materials (e.g. AETB, FRCI, SIRCA) include lack of structural stability at temperatures below=2800degrees F, high density (=12-20 lb/ft3/), and high cost (+$2.50-3.00/in3). The innovative TPS proposed in this project will provide an unequaled combination of structural and thermal properties, including temperature capability to >4500 degree F with outstanding erosion resistance. This TPS will combine Ultramet's lightweight, low-cost, low thermal conductivity (low-k) reticulated vitreous carbon (RVC) foam with aerogel insulation to reduce high temperature thermal conductivity and a frontside facesheet coating of refractory Ultra2000 TM, Ultramet's patented hafnium carbide/silicon carbide (HfC/SiC) coating system. Previous work has shown that the low-k RVC foam has comparable thermal conductivity to the current best insulators (AETB-12 and FRCI-12) with twice the compressive strength at temperatures of <1830degress F. At higher temperatures, radiative heat transfer within the foam results in rapid increases in thermal conductivity. The addition of low-density, low radiative heat transfer aerogels produced by Lawrence Livermore National Laboratory presents a novel approach to reducing radiative heat transfer with minimal increase in density and conductive heat transfer. In the proposed project, aerogels with be integrated with foam structures, and high temperature thermal conductivity will be measured to assess the feasibility of this novel concept.

* information listed above is at the time of submission.

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