Low-Cost Refractory Metal-Lined Graphite Components for Advanced SDACS

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$99,778.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
W9113M-10-P-0039
Award Id:
96939
Agency Tracking Number:
B093-003-0509
Solicitation Year:
n/a
Solicitation Topic Code:
MDA 09-003
Solicitation Number:
n/a
Small Business Information
12173 Montague Street, Pacoima, CA, 91331
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
052405867
Principal Investigator:
Victor Arrieta
Senior Research Engineer
(818) 899-0236
victor.arrieta@ultramet.com
Business Contact:
Craig Ward
Engineering Administrative Manager
(818) 899-0236
craig.ward@ultramet.com
Research Institute:
n/a
Abstract
Rhenium hot gas path components are used extensively in the solid divert and attitude control system (SDACS) of the MDA/Navy Standard Missile-3 Aegis LEAP Interceptor missile defense program, on which Ultramet is a key subcontractor. The mechanical, thermal, and chemical performance of rhenium is unmatched. However, a need clearly exists to reduce the cost and weight of rhenium-based structures for advanced SDACS such as that being developed for MDA by Valley Tech Systems. In previous and current work, Ultramet has demonstrated the potential for fabrication of refractory metal-lined low-density graphite components, sometimes in combination with a carbon diffusion barrier interlayer. The potential exists to apply this same technology for the fabrication of hot gas valve and thruster components for use in advanced SDACS systems. The combination of materials will potentially allow the benefits of flight-qualified rhenium to be retained while offering substantially reduced weight and cost. In this project, Ultramet will team with Valley Tech Systems to demonstrate the feasibility of rhenium-lined graphite as an alternative to monolithic rhenium structures for SDACS. Ultramet's current manufacturing contract for SM-3 components, as well as flight-qualified thrust chambers used in commercial satellite propulsion systems, makes it well-suited for the proposed development and demonstration of lower cost and lighter weight rhenium-based components.

* information listed above is at the time of submission.

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