Effects of oxidizing additives on the physical properties and ignition performance of hydrogen peroxide-based hypergolic propellants

Author:

Park Seonghyeon,Lee Kyounghwan,Kang HongjaeORCID,Park Youngchul,Lee Jongkwang

Funder

Agency for Defense Development

Defense Acquisition Program Administration

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Advances in hypergolic propellants: ignition, hydrazine, and hydrogen peroxide research;Davis;Adv. Aerosp. Eng.,2014

2. Green comparable alternatives of hydrazines-based monopropellant and bipropellant rocket systems;Hasan,2019

3. Hypergolic propellants based on hydrogen peroxide and organic compounds: historical aspect and current state;Guseinov;Bull. Acad. Sci. USSR, Div. Chem. Sci.,2018

4. Suppression of hard start for nontoxic hypergolic thruster using H2O2 oxidizer;Kang;J. Propul. Power,2017

5. Hypergolic reaction mechanisms of catalytically promoted fuels with rocket grade hydrogen peroxide;Pourpoint;Combust. Sci. Technol.,2007

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