Erratum to: Combustion characteristics of a hydroxylammonium nitrate based liquid propellant. Combustion mechanism and application to thrusters

T. Katsumi^a, H. Kodama^a, T. Matsuo^b, H. Ogawa^c, N. Tsuboi^c, K. Hori<sup>c

a</sup> 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

Language: English

 English version: Combustion, Explosion and Shock Waves, 2009, 45:5, 634