Liquid propellant rocket engine cycles partially using electric turbopump

Autor: Shoyama, Tadayoshi, Wada, Yutaka, Shimagaki, Mitsuru, Hashimoto, Tomoyuki, Takada, Satoshi
Zdroj: In Acta Astronautica November 2024 224:138-147
Databáze: ScienceDirect