Integrated Optimization for Single-Stage-to-Orbit Using a Pulse Detonation Engine.
Autor: | Hiroaki Yoshida1, Micci, Michael M.2, Masakatsu Nakane3, Katsuhito Yamaguchi4, Yoshio Ishikawa5 |
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Zdroj: | Journal of Spacecraft & Rockets. Jul2019, Vol. 56 Issue 4, p983-989. 7p. |
Databáze: | Academic Search Ultimate |
Externí odkaz: |