New HAN-based mixtures for reaction control system and low toxic spacecraft propulsion subsystem: Thermal decomposition and possible thruster applications

2015/04/18 by Rachid Amrousse, Toshiyuki Katsumi, Noboru Itouyama +5 · 7 citations
Engineering · #Rocket and propulsion systems research #Energetic Materials and Combustion #Electrohydrodynamics and Fluid Dynamics

paper · doi:10.1016/j.combustflame.2015.03.026

Cited by

• Impact of MWCNT/Al on the combustion behavior of hydroxyl ammonium nitrate (HAN)-based electrically controlled solid propellant
• Controllable ignition, combustion and extinguishment characteristics of HAN-based solid propellant stimulated by electric energy
• Influence of metal addition on flame structure and potential instability in solid propellant combustion driven by electric potential
• Co-Electrolysis-Assisted Decomposition of Hydroxylammonium Nitrate-Fuel Mixtures Using Stainless Steel-Platinum Electrodes. [europepmc]
• Cerium oxide based active catalyst for hydroxylammonium nitrate (HAN) fueled monopropellant thrusters. [europepmc]
• Experimental Studies on Parametric Effects and Reaction Mechanisms in Electrolytic Decomposition and Ignition of HAN Solutions. [europepmc]
• Ammonia (NH 3 ) Production from the Thermal Decomposition of Hydroxylammonium Nitrate (HAN) as a Green Energetic Source for Clean Space. [europepmc]