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Decomposition Characterization and Optimization for Monopropulsion Systems for Spacecraft

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: F04611-03-M-3007
Agency Tracking Number: O031-0172
Amount: $99,997.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Timeline
Solicitation Year: N/A
Award Year: 2003
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
300 Westdale Avenue
Westerville, OH 43082
United States
DUNS: 877299446
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Richard Sapienza
 Senior Scientist
 (614) 797-2200
 rsapienza@metss.com
Business Contact
 Kenneth Heater
Title: President
Phone: (614) 797-2200
Email: kheater@metss.com
Research Institution
N/A
Abstract

This program seeks to develop a means of initiating a repeatable, reliable exothermic decomposition of USAF developed high performance Hydroxyl Ammonium Nitrate (HAN) based monopropellants, over a range of demanding mission duty cycles with short delaytimes and predictable performance over long storage times. Catalysts do not have the high temperature or oxidation resistance required by these USAF developed HAN based monopropellants to support the program objectives. However, these materials should besusceptible to initiation, or self-sustained energy release, when present in sufficient quantities and exposed to stimuli such as heat, shock, friction, chemical incompatibility, or electrostatic discharge. Under the proposed program, METSS proposes toconduct a study to develop an initiator/sensitizer for HAN based monopropellants by exploiting the exothermic decomposition properties of the amine nitrates. Furthermore, METSS will demonstrate that the formulations synthesized under this program willdecompose HAN at concentrations of 2-5%. Chemicals dispersed with the fuel will react with one another or the fuel over a nozzle structural surface generating heat from the reaction sufficient to either start or speed up the monopropellant decompositionreaction. The chemical initiator composition will be selected for specific characteristics: high thermal stability, fast response, sustained thermal output, and high short-term peak energy. Specifically, the work will emphasize the pre-existingtechnologies of azo polymer initiators and the reduction of nitrate by an added reducing agent, and recent developments that can convert nitrate in water into environmentally benign gaseous nitrogen. METSS believes that high activity, low cost initiatorscan be developed using this approach that will decompose the HAN fuel. This project will demonstrate a complete, cost effective technology. In addition to military interests, there is a wide range of commercial uses for HAN, ranging from pharmaceuticalproducts to re-processing nuclear fuels. A versatile chemical, HAN can also be used as an oxidizer or reducing agent in applications such as photographic developing, semiconductor manufacturing and as a high performance fuel additive, propellant or gasgenerator for mining, boring and other operations. The use of existing commercially available processing equipment and the existing commercial market make the transition of this methodology into the commercial environment technically and financiallyfeasible.

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

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