Dual control over the reignition and combustion performance of hydroxylammonium nitrate-based gel propellants

Author:

Chun-tian Li,Zi-yang Lu,Zhi-wen Wang,Lian Li,Zhi-dong Wang,Yu-cheng Zhang,Rui-qi ShenORCID,De Luca Luigi T.,Zhang WeiORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference28 articles.

1. Modular impulsive green-monopropellant propulsion system for micro/nano satellites high-thrust orbital maneuvers (MIMPS-G);Nosseir,2020

2. A review on hydroxylammonium nitrate (HAN) decomposition techniques for propulsion application;Chai;Acta Astronaut,2022

3. A review on surface coating strategies for anti-hygroscopic of high energy oxidizer ammonium dinitramide;Yang;Defence Tech,2023

4. Fabrication and preliminary testing of hydroxylammonium nitrate (HAN)-based ceramic microthruster for potential application of nanosatellites in constellation formation flying;Markandan;Microsyst Technol,2019

5. HAN and ADN as liquid ionic monopropellants: thermal and ctalytic decomposition processes;Amrousse;Appl Catal B Environ,2012

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