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Erratum to: Combustion characteristics of a hydroxylammonium nitrate based liquid propellant. Combustion mechanism and application to thrusters
T. Katsumia, H. Kodamaa, T. Matsuob, H. Ogawac, N. Tsuboic, K. Horic a University of Tokyo, Tokyo, Japan
b Mitsubishi Heavy Industries, Ltd., Nagasaki, Japan
c Institute of Space and Astronautical Sciences, Kanagawa, Japan
Received: 25.10.2008 Accepted: 11.08.2009
Citation:
T. Katsumi, H. Kodama, T. Matsuo, H. Ogawa, N. Tsuboi, K. Hori, “Erratum to: Combustion characteristics of a hydroxylammonium nitrate based liquid propellant. Combustion mechanism and application to thrusters”, Fizika Goreniya i Vzryva, 45:5 (2009), 143; Combustion, Explosion and Shock Waves, 45:5 (2009), 634
Linking options:
https://www.mathnet.ru/eng/fgv1361 https://www.mathnet.ru/eng/fgv/v45/i5/p143
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