新型液体火箭发动机试车台起动试验系统方案设计  

Tentative design of starting test system for new liquid rocket engine test bed

作　　者：耿文忠[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》2008年第3期49-53,共5页Journal of Rocket Propulsion

摘　　要：为满足总体对发动机地面试验入口压力的设计要求,提出了三种试车台起动试验系统设计方案。论证表明,设计方案可行,布局紧凑、合理。综合考虑,确定起动容器与主容器接力试验系统作为新建台的设计方案。To meet the engine ground test inlet pressure design requirements of the general proposal and the design task document. Three tentative designs of starting test system of the test bed were proposed and their feasibilities were proved. Upon the construction document of the new test bed, the optimum design of starting tank with the combination of compact layout and the reasonable structure design was stated in this paper. The new design of starting test system of the test bed meets the general design proposal requirements on the engine ground starting test, and provides the experience for the future test bed building.

关 键 词：试车台 发动机起动试验 方案设计 

分 类 号：V434[航空宇航科学与技术—航空宇航推进理论与工程]