导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
Missiles and Space Vehicles
2015年
6期
21-24,45
,共5页
25吨级膨胀循环发动机%推力室%氢涡轮泵%关键技术
25噸級膨脹循環髮動機%推力室%氫渦輪泵%關鍵技術
25둔급팽창순배발동궤%추력실%경와륜빙%관건기술
25t expander cycle%Thrust chamber%Hydrogen turbopump%Key technology
通过推算国外20吨级氢氧膨胀循环发动机系统参数,获得发动机系统的关键特征,介绍25吨级膨胀循环发动机系统方案设置,通过参数平衡优化及最低夹套温升条件限制,提出25吨级膨胀循环发动机主要性能参数,并简要介绍了推力室、氢涡轮泵两大核心组件技术方案及其它需开展的关键技术.
通過推算國外20噸級氫氧膨脹循環髮動機繫統參數,穫得髮動機繫統的關鍵特徵,介紹25噸級膨脹循環髮動機繫統方案設置,通過參數平衡優化及最低夾套溫升條件限製,提齣25噸級膨脹循環髮動機主要性能參數,併簡要介紹瞭推力室、氫渦輪泵兩大覈心組件技術方案及其它需開展的關鍵技術.
통과추산국외20둔급경양팽창순배발동궤계통삼수,획득발동궤계통적관건특정,개소25둔급팽창순배발동궤계통방안설치,통과삼수평형우화급최저협투온승조건한제,제출25둔급팽창순배발동궤주요성능삼수,병간요개소료추력실、경와륜빙량대핵심조건기술방안급기타수개전적관건기술.
Based on the feature study of a foreign 20t class LOX/LH2 expander cycle engine, the system scheme of a 25t expander cycle engine is put forward. The main performance parameters of the 25t expander cycle engine are promoted by optimizing balance parameters and restricting the condition of the lowest temperature raise in the jacket. Also, the technology schemes of the thrust chamber and the hydrogen turbopump, together with other key technologies are briefly introduced.
