The green propellant
hydroxylammonium nitrate (HAN) is a good alternative
to the conventional propellants in space propulsion applications because
of its low toxicity and high energy density. Electrolytic decomposition
and ignition of HAN solution, an ionic liquid, is a promising approach.
In this work, comprehensive experimental studies were conducted to
examine effects of different electrolytic voltages, electrode surface
areas, and HAN concentrations on the decomposition process. In the
test cases, an optimum electrolytic voltage appears to exist, which
leads to the fastest decomposition process. As the voltage increases,
a larger electrode surface area on the anode side should be used to
overcome an anodic inhibition phenomenon and accelerate the electrolytic
process. A high concentration of HAN solution is preferred for its
decomposition and ignition. Results also reveal that the electrolytic
process of a HAN solution could eventually trigger thermal decomposition
reactions, raising the maximum temperature to around 550 K at the
final stage. A detailed chemical reaction mechanism was proposed,
based on the experimental data and FTIR spectra analyses. Results
obtained herein would provide fundamental understandings on the complex
electrochemical and physical processes and should be helpful for future
applications of the electrolytic decomposition and ignition technology.