SÄNGERⅡ高超声速计划推进系统综述  

Overview of propulsion for SÄNGER Ⅱ hypersonic program

作　　者：陈玉洁 娄德仓 孙杉 钟世林 邓远灏 李丹 CHEN Yu-jie;LOU De-cang;SUN Shan;ZHONG Shi-lin;DENG Yuan-hao;LI Dan(AECC Sichuan Gas Turbine Establishment,Chengdu 610500,China;Unit 93160 of Chinese People's Liberation Army,Beijing 100074,China)

机构地区：[1]中国航发四川燃气涡轮研究院,成都610500 [2]中国人民解放军93160部队,北京100074

出　　处：《燃气涡轮试验与研究》2023年第1期54-62,共9页Gas Turbine Experiment and Research

摘　　要：介绍了世界上首次针对涡轮冲压组合循环动力开展深入论证和试验的德国桑格尔(SÄNGER Ⅱ)高超声速计划。详细阐述了SÄNGER Ⅱ空间运输系统的总体设计、两级入轨推进系统方案的关键技术及其验证、飞发一体化、热管理系统和二动力系统。尽管因各种原因,SÄNGER Ⅱ高超声速计划未能成功现实,但借助该计划研发了大量的先进技术,且在高超声速飞行器设计方案、分析方法、试验验证等方面都取得了宝贵的经验,可为我国组合动力及其他高超声速工程研制提供参考。Germany SÄNGER Ⅱ hypersonic program was introduced,which was the first program to carry out demonstration tests on turbine-based combined cycle engine in the world.General design of SÄNGER Ⅱ space transportation system,key technologies of two-stage-to-orbit propulsion system and verification tests,aircraft/engine integration,thermal management and secondary power system were illustrated in detail.Though SÄNGER Ⅱ hypersonic program wasn’t complete for various reasons,a lot of advanced technologies were developed under it.And precious experience was obtained on the aspects of hypersonic aircraft scheme design,analysis methods and test verification which could be referential for development of combined cycle engine and other hypersonic engineering application in China.

关 键 词：SÄNGERⅡ计划 空天飞机 推进系统 两级入轨 热管理 二动力 飞发一体化 

分 类 号：V23[航空宇航科学与技术—航空宇航推进理论与工程]