HTPB TYPE COMPOSITE SOLID PROPELLANT

• 1. 一种工艺性能改善的高固含量DDI-HTPB推进剂及其加工工艺 [P] . 中国专利： CN109651027B . 2021.03.23
• 2. 一种HTPB基大分子钝感剂及其制备方法和应用 [P] . 中国专利： CN112552132B . 2021.09.28
• 3. Bonding agents for HTPB-type solid propellants [P] . 美国专利： US5417895A . 1995-05-23

  机译： HTPB型固体推进剂的粘结剂

• 4. Process and apparatus for the preparation of a composite-type solid propellant paste [P] . 欧洲知识产权局专利： EP1652574A3 . 2010-12-01

  机译： 制备复合型固体推进剂糊的方法和设备

• 5. SOLID-PROPELLANT ROCKET ENFINE CASE FROM "COCOON'-TYPE COMPOSITE MATERIALS [P] . 俄罗斯专利： RU2327050C2 . 2008-06-20

  机译： “茧”型复合材料的固体推进剂火箭发动机箱

• 1. 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
• 2. Comparison of burn rate and thermal decomposition of AP as oxidizer and PVC and HTPB as fuel binder based composite solid propellants [J] . A.Manash, P.Kumar 兵工学报（英文版） . 2019,第002期
• 3. Light weight HTPB-clay nanocomposites(HCN)with enhanced ablation performance as inhibition materials for composite propellant [J] . Kavita Ghosh, L.V. Gaikwad, R.K. Kalal, 兵工学报（英文版） . 2021,第002期
• 4. 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
• 5. Developing a Viscoelastic Relaxation Model for AP-HTPB Composite Solid Propellant Based on Experimental Data [C] . Walid M. Add, LIANG Guo-zhu AIAA international space planes and hypersonic systems and technologies conference . 2017
• 6. 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
• 7. Dynamic Mechanical Response and Damage Mechanism of HTPB Propellant under Impact Loading [O] . Hengning Zhang, Meng Liu, Yinggang Miao, 2020
• 8. DEKOMPOSISI TERMAL PROPELAN KOMPOSIT BERBASIS AMONIUM PERKLORAT/HYDROXY TERMINATED POLYBUTADIENE (AP/HTPB) (THE THERMAL DECOMPOSITION ANALYSIS OF AMMONIUM PERCHLORATE/HYDROXYTERMINATED POLYBUTADIENE (AP/HTPB) COMPOSITE SOLID PROPELLANT) [O] . Wiwiek Utami Dewi, Yulia Azatil Ismah 2018
• 9. Study of the Gas Phase Chemistry of Solid Propellants Using a Microprobe Mass Spectrometer (MPMS) System: Preliminary Results for Solid Fuels (HTPB/Zecorez and BAMO/NMMO), Single-Base Propellant (M10) and an RDX-Based Propellant (BLX-9). [R] . Litzinger, T. A. 1991

• 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. M准则的修正及其在HTPB复合固体推进剂中的应用 [C] . 强洪夫 ,曹大志 ,张亚 . 中国宇航学会固体火箭推进24届年会 . 2007
• 3. HTPB/MDI型聚氨酯弹性体的分子动力学模拟 [A] . 崔慧娜 . 2018