SOLID PROPELLANTS CONTAINING BURNING RATE DEPRESSANTS

• 1. 生产固体含铝复合推进剂的方法以及固体含铝复合推进剂 [P] . 中国专利： CN102471175B . 2014.11.05
• 2. 生产固体含铝复合推进剂的方法以及固体含铝复合推进剂 [P] . 中国专利： CN102471175A . 2012-05-23
• 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. Composite propellant containing burning rate depressant and method of use [P] . 美国专利： US3026672A . 1962-03-27

  机译： 含燃速降低剂的复合推进剂及其使用方法

• 5. Positive displacement control system for controlling the flow of gases within a solid-propellant rocket motor to regulate the burning rate of the solid propellant [P] . 美国专利： US3418811A . 1968-12-31

  机译： 正排量控制系统，用于控制固体推进剂火箭发动机内的气体流量，以调节固体推进剂的燃烧速率

• 1. 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
• 2. 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
• 3. 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
• 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. Multidimensional modeling of solid propellant burning rates and aluminum agglomeration and one-dimensional modeling of RDX/GAP and AP/HTPB. [D] . Tanner, Matthew W. 2008
• 6. Single-Walled Carbon Nanotubes (SWCNTs) as Solid-Contact in All-Solid-State Perchlorate ISEs: Applications to Fireworks and Propellants Analysis [O] . Saad S. M. Hassan, Ahmed Galal Eldin, Abd El-Galil E. Amr, 2019
• 7. A study of the burning rates of composite solid propellants in acceleration fields. [O] . Sturm Edward John 1968
• 8. Effects of Propellant Composition Variables on Acceleration-Induced Burning-Rate Augmentation of Solid Propellants [R] . Northam, G. B. 1972

• 1. 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
• 2. 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
• 3. AP复合固体推进剂含能降速剂的研究 [C] . 柳先玮 ,张炜 . 中国航空学会动力分会火箭发动机专业委员会2010年推进技术学术年会 . 2010
• 4. 含缺陷固体火箭发动机推进剂断裂力学行为研究 [A] . 周广盼 . 2013