Firing Tests and Simulations of a CubeSat-Scale H 2 O 2 -Based Hybrid Rocket
Year: 2025
Type: article
Source: Journal of Propulsion and Power
DOI: 10.2514/1.b39941
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4417093760
