K Zhang, F Qin, X Yu, S Zhu, D Zhang - Acta Astronautica, 2024 - Elsevier
The Mach 6-capable turbine based combined cycle engine is a potential first-stage propulsion for TSTO mission. In order to improve thrust-to-weight ratio, an innovative tandem …
S Nie, F Qin, J Ye, X Wei, G He - Acta Astronautica, 2025 - Elsevier
One of the principal research subjects within the field of rocket-based combined cycle (RBCC) engines has been the ejector mode, which has been the focus of research for a …
S Nie, G He, J Ye, X Wei, F Qin, S Zhu - Aerospace Science and …, 2024 - Elsevier
Variable geometry combustor technology is a novel technical approach for enhancing the performance of rocket-based combined cycle (RBCC) engines. This research paper …
QIN Fei, Z Zheng, HE Guoqiang, J Tingting… - Acta Aeronautica et …, 2024 - sciopen.com
As one of the principal propulsion systems for the development of future horizontal take-off and landing reusable earth-to-orbit transportation systems and near-space high-speed flight …