SBIR/STTR Research Award

CRACKED AMMONIA FOR HYPERSONIC PROPULSION

Award identifier 170d536a786a50c89b59223cb779ec1e015ea0b19367c42402ba4156e562ee11Awarding agency Department of Defense · Air Force

Award amount

$62,834

Program and phase

SBIR · Phase I

Award year

1987

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Energy Science Laboratories, Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

CRACKED AMMONIA (NITROGEN + HYDROGEN, 3H(2)+N(2)) HAS MANY ADVANTAGES AS A HYPERSONIC PROPULSION FUEL. IT HAS GOOD HEAT SINK CAPACITY, AND A GOOD VOLUMETRIC HEATING VALUE COMPARED TO LIQUID HYDROGEN. IT ALSO HAS MANY OTHER CONVENIENT PROPERTIES COMPARED TO LIQUID HYDROGEN. WE PROPOSE TO STUDY THE SYSTEMS ADVANTAGES OF AMMONIA VS. HYDROGEN FUEL, THE HEAT TRANSFER AND (CATALYZED) CRACKING KINETICS APPLICABLE TO ITS USED AS A COOLANT, AND CERTAIN ASPECTS OF ITS BEHAVIOR AS A FUEL GAS FOR SUPERSONIC COMBUSTORS.

Technology keywords

Not reported

Agency intelligence

Department of Defense

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