4JANKOVSKY R S. HAN-based monopropellant assessment for spaeecraft, AIAA 96-2863[R]. 1996.
5ANFLO K. Development and testing of ADN-based monopropellants in small rocket engines,AIAA-2000-3162[R]. 2000.
6FOKEMA M D,TORKELSON J E. Thermally stable catalysts and process for the decomposition liquid propellants: US, 20080064914[P]. 2008.
7FORTINI A J. Self-adjusting catalyst for propellant decomposition : US, 20080064913[P]. 2008.
8HAWKINS T W. Reduced toxicity, high performance monopropellant at the U. S. Air Force Research Laboratory [C]. 4th International Association for the Advancement of Space Safety Conference. Huntsville, AL : AFRL, 2010 : 1 -- 8.
9VOSEN S R. Hydroxylammonium nitrate-based liquid propellant combustion-interpretation of strand burner data and the laminar burning velocity[J]. Combustion and Flame, 1990, 82(3--4) ,376--388.
10MCBRATNEY W F, VANDERHOFF J A. High pressure windowed chamber burn rate determination of liquid propellant XM46, ARL-TR-442[R]. 1994.
