Reduction of Aerodynamic Interference for Separation of Two-Stage Reuseable Launch Vehicles

Author:

UEMATSU Taro1,ISHIDA Takuro1,ASO Shigeru1,TANI Yasuhiro1

Affiliation:

1. Kyushu University

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 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. Unsteady investigation on parallel separation for spiked two-stage reusable launch vehicle;Chinese Journal of Aeronautics;2023-11

2. Aerodynamic Interference Reduction Using Aerospike for Two-Stage Reusable Launch Vehicle;Journal of Aerospace Engineering;2023-07

3. Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle;Journal of Spacecraft and Rockets;2023-01

4. Aerodynamic Study of the Parachute Container Hatch Door with Various Design Parameters in its Separation from the Reentry Vehicle;Proceedings of Higher Educational Institutions. Маchine Building;2022-02

5. Numerical analysis of the descent module and its bottom structure element aerodynamic characteristics during their separation;XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2021

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