Low-Cost Processing of Liners for Zero-Eroding Nozzles

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$70,000.00
Award Year:
2002
Program:
SBIR
Phase:
Phase I
Contract:
N00178-02-C-2034
Award Id:
58720
Agency Tracking Number:
02-1165
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
2721-D Merrilee Drive, Fairfax, VA, 22031
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
167433531
Principal Investigator:
T.S. Sudarshan
Vice-President & COO
(703) 560-1371
sudarshan@matmod.com
Business Contact:
T.S. Sudarshan
Vice-President & COO
(703) 560-1371
sudarshan@matmod.com
Research Institute:
n/a
Abstract
"After September 11, 2001, Missile Defense has taken on a significantly higher national priority for the protection of the US homeland and territories of allies, as well as other important national assets. Missiles currently in development such as theTHAAD, NMD, Standard Missile 3, or SM3, are multiple stage missiles designed to achieve the required range concurrent with the ability to impart the velocity (or kinetic energy) needed to destroy the target with a hit-to-kill strategy. Current boostermotor (or "axial" boost propulsion) nozzles use costly carbon-carbon (C-C) composites or expensive and complex, multi-part (3-D) nozzles with forged tungsten inserts to achieve the high booster motor performance required. Development of a zero-erosionnozzle liner would enable significantly lower nozzle cost concomitant with a significant reduction in the cost of the propulsion system. MMI proposes a low-cost synthesis technique in conjunction with a fast processing technique for the fabrication ofhigh payoff, lower cost nozzle liner materials. The development of the methodology suggested in this proposal will significantly increase the options for the boost propulsion designer and will minimize or eliminate the use of costly C-C and expensivemulti-part forged tungsten based nozzles. commercial applications include:¿ Scramjet and ramjet turbine component¿ Reusable heat shields for reentry vehicle nosecones¿ Flame nozzles¿ Wa

* information listed above is at the time of submission.

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