整体式固体火箭冲压发动机研制

推进技术 ›› 1998, Vol. 19 ›› Issue (2): 10-14.

整体式固体火箭冲压发动机研制

张家骅,胡顺楠,顾炎武,曹中俄

航天工业总公司３１所;航天工业总公司３１所;航天工业总公司３１所;航天工业总公司３１所

发布日期:2021-08-15

DEVELOPMENT OF AN INTEGRAL SOLID ROCKET RAMJET ENGINE

The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074;The 31st Research Inst.,Beijing,100074

Published:2021-08-15

摘要/Abstract

摘要： 概要介绍了我国第一种整体式固体火箭冲压发动机试验研究样机的研制，讨论了样机地面试验研究和飞行试验研究两大阶段中，整机（含主级和助推级）、各部件及分系统的设计、试制和试验工作。样机结构合理，主级比冲比国外同类型号导弹发动机有较大提高，助推级综合性能和热防护技术也优于后者。

关键词: 整体式火箭冲压发动机;发动机设计;推进系统试验

Abstract: An integral solid rocket ramjet engine in China is introduced.The design,manufacture and test of the whole engine(both sustainer and booster),components and sub systems during ground and flight test phases were described.The test results show that this prototype was reasonable,the specific impulse of cruise stage was higher than that similar to engines abroad,and the integrated booster performance and thermal protection technique were satisfactory

Key words: Integral rocket ramjet;Engine design;Propulsion system test

张家骅,胡顺楠,顾炎武,曹中俄. 整体式固体火箭冲压发动机研制[J]. 推进技术, 1998, 19(2): 10-14.