Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology

Hangkong bingqi

Liu Ying, Lu Ning, Shen Xin¹ 

[1] 1. China Airborne Missile Academy, Luoyang 471009, China;

关键词: |integral solid rocket ramjet engine|patent|gas flow|propellant|thermal protection|aerodynamic profile;   

DOI  :  10.12132/ISSN.1673-5048.2020.0166

来源: DOAJ

【 摘 要 】

Missile power plant is a key factor in determining the missile’s range. This paper analyzes and discusses the current patented technologies and application status of integrated solid rocket ramjet engines in foreign countries (USA, Russia, Europe). Based on the analysis, the key technologies for the development of integrated solid rocket ramjet are summarized, mainly including gas flow regulation and control, high-energy oxygen poor propellant, thermal strength of structure and long-term thermal protection, wide range adjustable intake and exhaust, integrated aerodynamic shape design of missile and engine, etc.

【 授权许可】

Unknown