Study of Suborbital Rocket Plane Using Highly Pressurized Hydrogen/Nitrous Oxide
Year: 2025
Type: article
Source: Journal of Propulsion and Power
DOI: 10.2514/1.b39710
Authors: Takeshi Kanda, Kei Araki, Hidetaka Inagaki
Institution: Chubu University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Iwatani Naoji Foundation
OpenAlex ID: W4411282149
