Integrally Stiffened Carbon-Foam Core Hot Structure

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$70,000.00
Award Year:
2002
Program:
SBIR
Phase:
Phase I
Contract:
DASG60-02-P-0093
Agency Tracking Number:
02-0676
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
Allcomp, Inc.
209 Puente Ave., City of Industry, CA, 91746
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
026249487
Principal Investigator:
Wei Shih
President
(626) 369-4572
weishih@aol.com
Business Contact:
Wei Shih
President
(626) 369-1273
weishih@aol.com
Research Institution:
n/a
Abstract
"Allcomp proposes to design and develop innovative insulative carbon-foam cores for the hot structure of the next generation missiles and re-entry vehicles. Typical heatshield and re-entry structures encounter high heat flux and dynamic loads in theoperational environment. Conventional rib stiffened structure is structurally sound but thermally inadequate. The thick C-C rib provides a direct thermal path from outer skin to metallic under-structure and thus overheats the metal frame beyond its allowed servicelimit.Load-bearing insulative material offers a common solution for all hot structures. Combining the advances in carbon foam technology and composite processing, Allcomp proposes to develop a low cost methodology to produce stiffened structure using modularunits of carbon foam cores and C-C structural cells. In the proposed design, high strength, insulative carbon-foam briquetts(modules) will be encased in carbon fabric, and integrally bonded to produce a grid stiffened pattern. The grid dimensions, andthickness will be sized to sustain the operational mechanical and thermal design requirements. The continuous carbon-fabric bonding each of the adjacent foam modules provides the web of the grid-stiffened hot structure. Use of thin webs in the modulargrids will minimize heat transfer via the grid-webs. Furthermore, the grid-stiffened panels can be sized and stacked to provide desired core thickness, thus designed to s

* information listed above is at the time of submission.

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