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Erratum to: Combustion Characteristics of a Hydroxylammonium Nitrate Based Liquid Propellant. Combustion Mechanism and Application to Thrusters

机译：误诊：基于硝酸亚硝酸亚铵液推进剂的燃烧特性。燃烧机制和推进器的应用

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T. Katsumi; H. Kodama; T. Matsuo; H. Ogawa; N. Tsuboi; K. Hori;
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年度 2009
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1. Combustion Characteristics of a Hydroxylammonium Nitrate Based Liquid Propellant. Combustion Mechanism and Application to Thrusters [J] . T. Katsumi, H. Kodama, T. Matsuo Combustion, Explosion, and Shock Waves . 2009,第4期

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4. Numerical simulation of catalytic decomposition and combustion process in an hydroxylammonium nitrate (HAN)-based monopropellant thruster [C] . Yu Xiqiao, Lin Qingguo, Yao Tianliang International Astronautical Congress . 2017

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5. Combustion of Hydroxylammonium Nitrate Based Monopropellants [D] . Ferguson, Robert Edwin, II. 2021

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7. Design and Analysis of Combustion Chamber for HAN Based Mono Propulsion System Thruster for Spacecraft Application [O] . Naresh DC, Rudesh M 2020

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8. Theory of Combustion of Liquid Propellants Based on Hydroxylammonium Nitrate [R] . Williams, F. A. 1992

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Erratum to: Combustion Characteristics of a Hydroxylammonium Nitrate Based Liquid Propellant. Combustion Mechanism and Application to Thrusters

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