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Miniature Extendable Nozzles or actuating nozzles for improved ISP of DACS thrusters

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0147-13-C-7304
Agency Tracking Number: B122-022-0317
Amount: $149,964.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: MDA12-022
Solicitation Number: 2012.2
Solicitation Year: 2012
Award Year: 2013
Award Start Date (Proposal Award Date): 2013-02-25
Award End Date (Contract End Date): 2014-05-23
Small Business Information
350 Voyager Way
Huntsville, AL -
United States
DUNS: 839422763
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Joseph Sims
 Principal Investigator
 (256) 562-2191
Business Contact
 Rhonda Harrison
Title: Director, Contracts and Pricing
Phone: (256) 562-2123
Research Institution

ASI is pleased to team with ATK to present a novel concept for enabling large nozzle area ratio increases for future solid divert and attitude control system (SDACS) valves/thrusters. The proposed effort will demonstrate feasibility of this advanced concept through a thorough design study that includes mechanical layout and packaging, computational fluid dynamics (CFD) simulations of nozzle performance and a kill vehicle performance comparison. We anticipate those analyses will show quite significant kill vehicle divert performance increase. To support that conclusion for our proposal, we completed a survey of state of the art in extendible nozzles and used the relative performance rankings we found in the literature to determine whether our solution represents a significant advance in state of the art. That comparison shows that our proposed solution enables a two- to five-fold increase in area ratio (for the same length) over a fixed bell nozzle, and a 40% to 100% increase in area ratio over state-of-the-art extendible nozzles. Weight and reliability impacts are minimal.

* Information listed above is at the time of submission. *

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