为解决固体火箭冲压发动机和固体燃料冲压发动机的流量调节问题,曾经提出过采用固液燃气发生器的方案。近年来,意大利那不勒斯大学航天科学与工程系研究了两种固液燃气发生器方案,用控制固液燃烧来调节进入冲压燃烧室的富燃料燃气流量,从而达到调节固体火箭冲压发动机和固... In order to solve the problem of flow regulation of solid rocket ramjet and solid fuel ramjet engine, a solution using solid-liquid gas generator has been proposed. In recent years, the University of Naples Department of Aerospace Science and Engineering has studied two solid-liquid gas generator program, with the control of solid-liquid combustion to regulate the fuel-rich gas flow into the ramjet combustion chamber to achieve regulation of solid rocket ramjet and solid. .