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基于新一代战术导弹的要求欧洲动力装置制造公司(SEP)在80年代对复合材料发动机壳体,隔热材料和喉衬材料以及推力矢量控制系统等技术进行了大量的预先研究和试验验证工作。在称为“CRAYON 发动机规划”的战术导弹复合材料固体火箭发动机研究计划中,提出并讨论了许多新方案和新技术。这项固体火箭发动机(SRM)计划是由法国国防部和 SEP 联合投资的,目的是研究具有非常大的长径比、高纵向刚性的壳体以及高的推进剂质量与惰性质量比的高性能复合材料固体火箭发动机。计划的主要验证项目包括:1)力学试验以及验证外壳的坚固度和评估材料的性能;2)厚壁试验以检测推力矢量控制系统和隔热材料的有效性;3)点火试验以逐步验证材料的性能和新方案的可行性。这些试验都是成功的,它为在战术导弹上应用新型固体火箭发动机以极大地提高其弹道性能开创了道路,而且某些技术也能用于弹道式固体火箭发动机,这方面的验证工作也在进行中。详细介绍了设计方案,进行的试验及试验后取得的数据和观察结果。
Based on the requirements of the new generation of tactical missiles European power plant manufacturing company (SEP) in the 1980s on the composite engine housing, insulation materials and throat lining material and thrust vector control systems and other technologies conducted a lot of pre-research and experimental verification. In a research project called “CRAYON Engine Planning” for a tactical missile composite solid rocket motor, many new solutions and new technologies were proposed and discussed. The Solid Rocket Engine (SRM) program is a joint venture between the French Ministry of Defense and the SEP to study housings with very large aspect ratios, high longitudinal rigidity, and high propellant mass to inert mass ratios Composite solid rocket motor. The main validation items planned include: 1) mechanical testing and verification of the firmness of the shell and evaluation of material properties; 2) thick wall tests to test the effectiveness of thrust vector control systems and insulation materials; and 3) ignition tests to verify the material The performance and feasibility of new programs. These tests were successful and opened the way for the application of new solid rocket motors to tactical missiles to greatly improve their ballistic performance, and certain techniques could also be applied to ballistic solid rocket motors, as is the verification effort processing. Described in detail the design, the test carried out and the data obtained after the test and observation.