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Ionic Monopropellant Compatibility Study

Completed TRL 4 (started at 1, targeting 4)

Description

High performance green monopropellants require means of detection and remediation of spills and residues. This project investigated color tests for spill detection and methods for remediation. Innovation was achieved using COTS test kits, and both fundamental and novel chemistry applied to the monopropellant ingredients. The second phase examined candidate materials for use in AF-M315E propulsion systems. Pairs of representative alloys, passivated and native, were immersed in AF-M315E at 71 °C for 31 d, fluid samples were periodically characterized and post-test materials and fluids were finally characterized. Typical corrosion studies use only the total time of immersion; this study also obtained interim data points. The image shows a surface treated alloy on the left and the untreated alloy on the right. Candidate hydrazine alternatives have been developed for spacecraft propulsion. The U.S. Air Force AF-M315E and the Swedish ammonium dinitramide propellants have received the most attention, while ammonium dinitramide propellants are a possible contender. While greenness relates to environmentally benign and relative toxicity, neither of these propellants is completely "nontoxic" or completely safe; if their energetic nature was not inherent they would not be used as monopropellants. This is particularly important with ammonium dinitramide (ADN) and hydrazinum nitroformate (HNF) propellants, which ESA and the EU has favored while the U.S. Air Force has focused on AF-M315E and the U.S. Army has investigated hydroxylammonium nitrate/triethanolammonium nitrate (HAN/TEAN; XM-46) propellants. The first phase of the project's focus will be to evaluate detection and decontamination methods for these propellants. The second phase examined candidate materials for use in AF-M315E propulsion systems. Pairs of representative alloys, passivated and native, were immersed in AF-M315E at 71 °C for 31 d, fluid samples were periodically characterized and post-test materials and fluids were finally characterized. Typical corrosion studies use only the total time of immersion; this study also obtained interim data points.

Benefits

Develop detection and decontamination methods for green ionic propellants on future manned spacecraft. The second phase will investigated material compatibility issues for AF-M-315E and will provide data for system engineers to use. DoD and commercial entities can use these methods and data. The JANNAF Propellant and Explosives Development and Characterization Subcommittee can be a forum for insertion into industry.

Details

Technology areaPropulsion Systems > Chemical Space Propulsion > Earth Storable Propellants
ProgramCenter Innovation Fund: JSC CIF (JSC CIF)
Lead organizationJohnson Space Center, Houston, TX
Start date2011-10-01
End date2012-09-01

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