[1]王新强,邓康清,李洪旭,等.电控固体推进剂点火技术研究[J].固体火箭技术,2017,40(03):313-318.[doi:10.7673/j.issn.1006-2793.2017.03.008]
 [J].Journal of Solid Rocket Technology,2017,40(03):313-318.[doi:10.7673/j.issn.1006-2793.2017.03.008]
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电控固体推进剂点火技术研究

参考文献/References:

[1]张淑慧,胡波,孟雅桃. 推力可控固体火箭发动机应用及发展[J]. 固体火箭技术, 2002, 25(4): 12-15.[2]Sawka W N, Katzakian A, Grix C. Solid state digital cluster thrusters for small satellites, using high performance electrically controlled extinguishable solid propellants[C]//19th Annual AIAA/USUSmall Satellite Conference, 2005.[3]Kimberly Chung, Eugene Rozumov. Development of electrically controlled energetic materials for 120 mm tank igniters[C]//Insensitive Munitions and Energetic Materials Technology Symposium , 2012.[4]Andrew Nicholas, Sawka Wayne N. SpinSat mission overview[C]//27th Annual AIAA/USU Conference on Small Satellites, 2013.[5]James K Baird, Joshua R Lang, Andrew T Hiatt. Electrolytic combustion in the polyvinyl alcohol + hydroxylammonium nitrate solid propellant[R]. AIAA 2016-4908. [6]Matthew S G, Joshua L R. Observation of late-time ablation in electric solid propellant pulsed microthrusters[R]. AIAA 2016-4845.[7]Wayne N Sawka, Michael Mc Pherson. Electrical solid propellants: a safe micro to macro propulsion technology[R]. AIAA 2013-4168.[8]Andrew T H, Robert A F. Laboratory experimentation and basic research investigating electric solid propellant electrolytic characteristics[R]. AIAA 2016-4935.

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更新日期/Last Update: 2017-06-29
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