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
Zdroj: Journal of Spacecraft & Rockets. Jul2019, Vol. 56 Issue 4, p983-989. 7p.
Databáze: Academic Search Ultimate