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Aluminum Borohydride Ammines as Fuels for Hybrid Rocket Motors: Theoretical Performance and Particle SynthesisThe aluminum borohydride ammines, Al(BH4)3·XNH3, are a family of complexes between aluminum borohydride and ammonia for which up to six moles of ammonia can be complexed per mole of aluminum borohydride. Two of these complexes, the diammine (X = 2) and hexammine (X = 6) are of particular interest for use in hybrid rocket motors as additives and stand alone fuels. This study compares these compounds against other metal hydride for their potential as additives to increase the regression rate of solid fuel grains. The theoretical performance of the diammine as a stand alone fuel paired with non-toxic oxidizers is also investigated. The low temperature and good performance of these combinations make them of interest for low cost orbital maneuvering thrusters. Finally, the synthesis process for Al(BH4)3·6NH3 is discussed and TGA/DSC results are presented.
Document ID
20220006969
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
D L Drewniak
(Pennsylvania State University State College, Pennsylvania, United States)
J E Boyer
(Pennsylvania State University State College, Pennsylvania, United States)
R A Yetter
(Pennsylvania State University State College, Pennsylvania, United States)
Date Acquired
May 4, 2022
Subject Category
Propellants And Fuels
Meeting Information
Meeting: 69th JANNAF Propulsion Meeting (JPM)
Location: Newport News, VA
Country: US
Start Date: June 6, 2022
End Date: June 10, 2022
Sponsors: United States Department of the Army, United States Department of the Air Force, United States Department of the Navy, National Aeronautics and Space Administration
Funding Number(s)
CONTRACT_GRANT: 80NSSC21K1283
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
hybrid rockets
Aluminum Borohydride Ammines
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