共 50 条
- [1] Approach to decreasing the burning rate of NEPE propellant Guti Huojian Jishu/Journal of Solid Rocket Technology, 2002, 25 (02):
- [2] Study on burning-rate control of low burning-rate HTPB propellant Tuijin Jishu/Journal of Propulsion Technology, 1999, 20 (02): : 77 - 82
- [3] Study on the formulation of low burning rate HTPB propellant with RDX Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2009, 32 (05): : 54 - 57
- [4] Erosive burning model identification of a propellant with low burning rate Yuhang Xuebao/Journal of Astronautics, 2008, 29 (06): : 1932 - 1935
- [5] Effect of nitramine on energy and burning rate of low burning rate HTPB propellant Guti Huojian Jishu/Journal of Solid Rocket Technology, 2001, 24 (02): : 45 - 47
- [6] Relationship between the characteristic value of PDSC and burning rate of NEPE propellant containing CL-20 Hanneng Cailiao/Chinese Journal of Energetic Materials, 2008, 16 (03): : 315 - 318
- [7] Study on burning rate catalysis of ultra-high burning rate propellant Shiyou Daxue Xuebao/Journal of the University of Petroleum China, 1998, 22 (05): : 91 - 94
- [9] Rheological Study on the Crosslinking of NEPE Propellant CHEMICAL JOURNAL OF CHINESE UNIVERSITIES-CHINESE, 2009, 30 (06): : 1230 - 1234
- [10] Process Performance of Low Aluminum and Low Burning Rate HTPB Propellant Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (03):