凝胶试验系统的设计及试后处理工艺  

Design of test system for gel propellants and processing measures after tests

作　　者：梁小强[1] 

机构地区：[1]西安航天动力试验技术研究所,陕西西安710100

出　　处：《火箭推进》2006年第4期51-53,共3页Journal of Rocket Propulsion

摘　　要：总结了凝胶发动机不同研制阶段相对应的试验系统以及系统试后处理工艺。包括以下几个方面:25N发动机试验系统的建立;变推力发动机试验系统的建立;双组元发动机试验系统的建立;变推力发动机试验系统的最终建立和凝胶试验系统试后处理工艺。通过对不同试验系统的建立与比较,确立了最终的凝胶试验系统及系统试后处理工艺。This article has summed up the design of the test system for gel propellants and the processing measures after tests during the different phases of the development of the gelled propellant. The test system of the engine of 25N, the test system of the engine of changeably thrust, the test system of the engine of two constitutes, the final test system of the engine of changeably thrust and the measures after trial of the test system were built up. After comparing the different test systems, the final test system of the gelled propellant and the measures after trial have been established.

关 键 词：凝胶 推进剂贮箱 试后处理工艺 

分 类 号：V416.6[航空宇航科学与技术—航空宇航推进理论与工程]