SBIR/STTR Research Award

Low Temperature Catalyst for Reduced Toxicity Monopropellant

Award identifier b58f469ca7ca594a1cee517480d966482d30d4175ca95d265a4e2d5d9bee5cc3Awarding agency Department of Defense · Army

Award amount

$70,000

Program and phase

SBIR · Phase I

Award year

2001

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
TDA RESEARCH, INC.
Proposal award date
Not reported
Contract end date
Not reported
UEI
MK5ANJVWVZK7
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Tactical missiles that use gel propellant systems require a chemical gas generator for pressurization. While hydrazine is a proven monopropellant for gas generation, it is poisonous, a cancer suspect agent, and has a high vapor pressure. As a result,full body protection and self-contained breathing apparatus (SCBA) are required during hydrazine loading procedures, non-essential personnel must leave the area, and hazardous material spill control teams have to be readily available. The result isincreased hazard expense and difficulty associated with the extensive safety procedures. New reduced-toxicity, non carcinogenic monopropellants are being developed by the Army for use in gas generators for tactical missile applications. Unfortunately,these new monopropellants will not ignite at the same low temperatures as hydrazine over existing catalysts. TDA Research Inc. (TDA), proposes to develop a catalyst that can ignite the new monopropellant at -40¿F. We will us our computer controlled,high-throughput, catalyst test apparatus to screen more than 100 promising low temperature catalytic formulations. A preliminary design of a gas generator that uses the new monopropellant and our catalyst will be designed by our commercializationpartner.TDA's catalysts will enable the use of the new, reduced-toxicity, non-hydrazine monopropellants for both gas generation and for monopropellant thrusters. Gas generation is used with missiles, spacecraft, and aircraft for pressurization andauxiliary power. Monopropellant thrusters are used on telecommunications and military satellites. In the case of thrusters, it has been estimated that every 1% increase in thruster efficiency made possible by the new generation of monopropellantsincreases total revenue by $1,000,000 per year per satellite (700+ satellites will be launched over the next decade). For gas generation, the ability to reduce the exposure of personnel to hydrazine provides a strong incentive to incorporate our catalytictechnology.

Technology keywords

Not reported

Research funding history

951 SBIR/STTR records share this UEI (1988–2026). Reported award amounts total $317,960,224. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, Environmental Protection Agency, National Science Foundation, Department of Health and Human Services

Agency intelligence

Department of Defense

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