Mono-Propellant Warm Gas Pressurization with Dual Use for Attitude Control System

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,903.00
Award Year:
2009
Program:
SBIR
Phase:
Phase I
Contract:
FA9300-09-M-3003
Agency Tracking Number:
F083-111-1206
Solicitation Year:
2008
Solicitation Topic Code:
AF083-111
Solicitation Number:
2008.3
Small Business Information
Systima Technologies, Inc.
1832 180th St. SE, Bothell, WA, 98012
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
086581902
Principal Investigator:
Aaron Freiheit
Sr. Mechanical Engineer
(425) 487-4020
aaron.freiheit@systima.com
Business Contact:
Tom Prenzlow
President
(425) 487-4020
tom.prenzlow@systima.com
Research Institution:
n/a
Abstract
Systima Technologies, Inc. is proposing an innovative self-pressurizing monopropellant supply system that eliminates the need for high-pressure propellant tanks and is capable of providing a constant pressure supply of propellant to conventional or multi-mode, monopropellant-based, propulsion systems.  Because the concept does not require high-pressure propellant tanks, the propellant tank weight can be minimized, resulting in significant weight savings.  In addition, since the propellant is not stored under high pressure, the propellant tanks can be shaped to the available space, not unlike the fuel tank in an automobile, dramatically increasing the packaging efficiency of the propellant tanks and reducing the overall size of the propulsion system. BENEFITS: The primary benefit expected from the Phase I and II programs is the design and development of a monopropellant supply system that is capable of providing a constant pressure supply of propellant to conventional and multi-mode propulsion systems and that is more compact and lower weight than conventional pressurization systems.  These attributes will make the technology attractive to manufacturers of satellites and satellite propulsion systems.

* information listed above is at the time of submission.

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