Feasibility Study of a DRBCC-Powered Single-Stage-To-Orbit Launch Vehicle

Author:

Zhang Fan,Zhang Huiqiang,Wang Bing

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Ascent guidance law for a horizontal take-off vehicle with a multi-combined cycle engine;Advances in Space Research;2020-01

2. Ascent trajectory optimization for air‐breathing vehicles in consideration of launch window;Optimal Control Applications and Methods;2019-10-28

3. The overall layout of rocket-based combined-cycle engines: a review;Journal of Zhejiang University-SCIENCE A;2019-03

4. Arrangement of Rocket Engine Location in a Combined Cycle Engine;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2019

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