Composite propellant containing burning rate depressant and method of use

• 1. 用于降低硝胺类推进剂压强指数的燃速催化剂 [P] . 中国专利： CN103212429A . 2013-07-24
• 2. 一种含聚二茂铁基化合物燃速促进剂的推进剂及其制备方法 [P] . 中国专利： CN101338236B . 2012.02.22
• 3. SOLID PROPELLANT CONTAINING STRONTIUM CARBONATE-CALCIUM CITRATE BURNING RATE DEPRESSANT [P] . 美国专利： US3841929A . 1974-10-15

  机译： 含碳酸锶-柠檬酸钙的固体推进剂燃速抑制剂

• 4. SOLID PROPELLANTS CONTAINING BURNING RATE DEPRESSANTS [P] . 美国专利： US3625782A . 1971-12-07

  机译： 含燃烧速率降低剂的固体推进剂

• 5. Ammonium perchlorate contg. burning moderator - for mfr. of relatively slow burning composite propellants or gas generators [P] . 德国专利： DE2353360A1 . 1975-05-07

  机译： 高氯酸铵（续）。刻录主持人-制造商。燃烧相对较慢的复合推进剂或气体发生器

• 1. Burning rate and other characteristics of strontium titanate (SrTiO3) supplemented AP/HTPB/Al composite propellants [J] . Sunil Jain, Garima Gupta, Dhirendra R.Kshirsagar, 兵工学报（英文版） . 2019,第003期
• 2. Effects　of　Metal　and　Composite　Metal　Nanopowders　on　the　Thermal　Decomposition　of　Ammonium　Perchlorate　（AP）　and　the　Ammonium　Perchlorate／Hydroxyterminated　Polybutadiene　（AP／HTPB）　Composite　Solid　Propellant [J] . 刘磊力, 李凤生, 谈玲华, 中国化学工程学报：英文版 . 2004,第004期
• 3. Application of transient burning rate model of solid propellant in electrothermal-chemical launch simulation [J] . Yan-jie NI, Yong JIN, Gang WAN, 兵工学报（英文版） . 2016,第002期
• 4. Experimental Study of Burning Rate Depressants Effect on the Burning Rate and Flame Temperature of DB Propellant [C] . QIN Neng, WANG Liang, WANG Ningfei, International Autumn Seminar on Propellants, Explosives and Pyrotechnics(2003 IASPEP); 20031015-18; Guilin(CN) . 2003
• 5. Methods of analysis of ultrasonic echoes to determine solid propellant burning rates [D] . Marshall, Marcus A. 2008
• 6. Preparation of Bi2O3/Al Core-Shell Energetic Composite by Two-Step Ball Milling Method and Its Application in Solid Propellant [O] . Min Xia, Qifa Yao, Huilian Yang, 2019
• 7. Tailoring the plateau burning rates of composite propellants by the use of nanoscale additives [O] . Stephens Matthew Aaron 2009
• 8. Refinement of Propellant Strand Burning Method to Suit Aluminised Composite Rocket Propellant. [R] . Smith, P. C., Hale, G., Pietrobon, R. A. 2014

• 1. Effects of Plasticizers,Antioxidants and Burning Rate Modifiers on Aging Performance of the HTPB/HMDI Composite Solid Propellant [J] . Ahmed M Enew ,Ehab Abadir ,Sahar Elmarsafy . 含能材料 . 2019,第001期
• 2. CALCHLATION OF BURNING RATE CHARACTERISTICS IN ACCELERATED FIELD FOR SOME ALUMINIZED SOLID PROPELLANTS [J] . 曹泰岳 . 国防科技大学学报 . 1995,第003期
• 3. 丁羟四组元低燃速推进剂降低燃速的方法研究 [C] . 高卫平 ,杜建锋 ,严伍启 . 中国航空学会火箭发动机专业委员会2014年火箭推进技术学术年会 . 2014
• 4. 高燃速复合固体推进剂燃速催化剂防迁移研究 [A] . 张家富 . 2005