Ignition and flow combustion characteristics of hydroxylammonium nitrate - based liquid propellant based on electric method

Author:

Jin Bao-zhi,Ma Jun-qiang,Li Guo-xiuORCID,Li Hong-meng

Funder

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference52 articles.

1. Green propulsion research at TNO The Netherlands;Mayer;Transactions on aerospace research,2018

2. Re-evaluation of rate constants for the reaction N2H4 (+ M) ⇄ NH2 + NH2 (+ M);Cobos;Combust. Flame,2022

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

4. Hydroxylammonium nitrate (HAN)-based green propellant as alternative energy resource for potential hydrazine substitution: from lab scale to pilot plant scale-up;Amrousse;Combust. Flame,2017

5. Research progress on ignition of HAN-based green propellant;Wang;Journal of Rocket Propulsion,2017

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