Experimental Characterization of a 5 N Hydrogen Peroxide Monopropellant Thruster Prototype

Author:

Pasini Angelo,Torre Lucio,Romeo Luca,Cervone Angelo,d'Agostino Luca,Musker Antony J.,Saccoccia Giorgio

Publisher

American Institute of Aeronautics and Astronautics

Cited by 18 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Experimental Assessment of the Pulse Mode Propulsive Performance of Small Chemical Thrusters;AIAA SCITECH 2024 Forum;2024-01-04

2. Firing Tests in Relevant Environment of a 500 mN HTP Thruster for CubeSat Applications;AIAA SCITECH 2024 Forum;2024-01-04

3. Engines on technical hydrogen peroxide as a platform for low-budget research of rocket and space technology;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

4. Hydrogen Peroxide Decomposition Catalysts Used in Rocket Engines;Russian Journal of Applied Chemistry;2020-04

5. Design and Test of a Hydrogen Peroxide Vapor Thruster for Small Satellite Applications;2018 Joint Propulsion Conference;2018-07-08

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