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介绍了现役导弹推进剂当前还不能满足法国官方文件──２０６０号ＤＧＡＩＰＥ规程规定的钝感弹药的全部要求，讨论了友合推进剂和低特征推进剂的新配方特性。并丁苯，这种含有被融聚的燃烧催化剂的预聚合物在使用温度范围内受热（或冲击）而不破坏其高能特性时可降低高燃速复合推进剂的敏感度和反应速度。对少烟推进剂而言，使用高能粘合剂对炸药填料（硝胺）的用量和高能增塑剂的敏感度都有一定限制以避免穿孔影响，而在性能上的某些损失是允许的。挤压式双基推进剂（ＳＤ１１７５，ＳＤ１１７８）的其它试验结果和燃器发生器推进剂试验说明，设计一种能够达到ＭＩＬ－ＳＴＳ２１０５钝感推进剂要求的发动机是可行的。可以肯定，不久将在新的高分子如六硝基六氮杂异伍兹（ＣＬ－２０），多叠氮基缩水甘油基和肼硝基甲酸盐研究领域将取得一些进展而使推进剂具有更好的性能和钝感水平。
The introduction of active missile propellants currently fails to meet all the requirements of the French official document - D Insensitive Munitions under the DGAIPE Code No.2060, and discusses the new formulation characteristics of both Union Helix and low-feature propellants. And styrene butadiene. Such a prepolymer containing the melt-fired combustion catalyst can reduce the sensitivity and the reaction rate of the high-burning-rate composite propellant when it is heated (or impacted) within the operating temperature range without breaking its high-energy characteristics. For less smoke propellants, the use of high energy binders imposes certain limits on the amount of explosive charge (nitramine) and the sensitivity of high energy plasticizers to avoid perforation effects, and some loss of performance is allowed . Additional test results for extruded double base propellants (SD1175, SD1178) and combustor generator propellant tests indicate that it is feasible to design an engine that meets the MIL-STS2105 needless propellant requirements. To be sure, some progress will soon be made in the field of new polymers such as hexanitrohexaazaisowurtzitane (CL-20), polyazide-substituted glycidyl and hydrazine-nitroformates to provide propellants with Better performance and sense of insecurity.