Shcramjet

A shock-induced combustion ramjet engine (abbreviated as shcramjet; also called oblique detonation wave engine; also called standing oblique detonation ramjet (sodramjet);^[1] or simply referred to as shock-ramjet engine) is a concept of air-breathing ramjet engine, proposed to be used for hypersonic and/or single-stage-to-orbit propulsion applications.^[2]

^ JIANG, Zonglin; ZHANG, Zijian; LIU, Yunfeng; WANG, Chun; LUO, Changtong (2021-03-01). "Criteria for hypersonic airbreathing propulsion and its experimental verification". Chinese Journal of Aeronautics. 34 (3): 94–104. doi:10.1016/j.cja.2020.11.001. ISSN 1000-9361.
^ "High Speed Vehicle Propulsion System Group". J. P. Sislian. Archived from the original on March 21, 2012.

[1] JIANG, Zonglin; ZHANG, Zijian; LIU, Yunfeng; WANG, Chun; LUO, Changtong (2021-03-01). "Criteria for hypersonic airbreathing propulsion and its experimental verification". Chinese Journal of Aeronautics. 34 (3): 94–104. doi:10.1016/j.cja.2020.11.001. ISSN 1000-9361.

[2] "High Speed Vehicle Propulsion System Group". J. P. Sislian. Archived from the original on March 21, 2012.

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