Constant Pressure Aerospike for Interceptor Axial Propulsion

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$99,982.00
Award Year:
2010
Program:
SBIR
Phase:
Phase I
Contract:
HQ0006-10-C-7304
Agency Tracking Number:
B093-001-0016
Solicitation Year:
2009
Solicitation Topic Code:
MDA09-001
Solicitation Number:
2009.3
Small Business Information
Analytical Services, Inc.
350 Voyager Way, Huntsville, AL, 35806
Hubzone Owned:
N
Socially and Economically Disadvantaged:
Y
Woman Owned:
N
Duns:
839422763
Principal Investigator:
Joe Sims
Principal Investigator
(256) 562-2191
joseph.sims@asi-hsv.com
Business Contact:
Rhonda Harrison
Director, Contracts and Pricing
(256) 562-2123
rhonda.harrison@asi-hsv.com
Research Institution:
n/a
Abstract
Our proposed effort will be used to determine the feasibility of a deeply-throttleable aerospike engine that maintains constant specific impulse performance, regardless of the throttle setting. The design incorporates technology previously demonstrated under another SBIR, but extends it through incorporation of an aerospike nozzle.

* information listed above is at the time of submission.

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