共 50 条
- [31] Synthesis of bismuth citrate and its effect on combustion of double-base propellant and RDX-CMDB propellant [J]. Binggong Xuebao, 2006, 4 (643-647):
- [33] OXIDIZER SIZE DISTRIBUTION EFFECTS ON PROPELLANT COMBUSTION [J]. AIAA JOURNAL, 1979, 17 (08) : 877 - 883
- [34] Measurement of Particle Size of Aluminum Combustion in Solid Propellant Using Digital In-line Holography [J]. Tuijin Jishu/Journal of Propulsion Technology, 2019, 40 (06): : 1399 - 1408
- [37] Effects of particle size of HMX/RDX on combustion characteristics of nitramine propellants under high and low pressure [J]. Guti Huojian Jishu/Journal of Solid Rocket Technology, 2010, 33 (03): : 319 - 322
- [39] The influence of particle size of RDX on the shock sensitivities of RDX/F2641 [J]. ISTM/2003: 5TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-6, CONFERENCE PROCEEDINGS, 2003, : 849 - 852
- [40] Study on the combustion properties of XLDB propellant [J]. Huozhayao Xuebao/Chinese Journal of Explosives and Propellants, 2001, 24 (04): : 50 - 51