Design and Validation of a Liquid Film-Cooled Hydrogen Peroxide/Kerosene Bipropellant Thruster. Jang, D., Kwak, Y., & Kwon, S. Journal of Propulsion and Power, 31(2):761–765, March, 2015. Number: 2 Publisher: American Institute of Aeronautics and Astronautics
Paper doi bibtex @article{jang_design_2015,
title = {Design and {Validation} of a {Liquid} {Film}-{Cooled} {Hydrogen} {Peroxide}/{Kerosene} {Bipropellant} {Thruster}},
volume = {31},
issn = {0748-4658},
url = {https://arc.aiaa.org/doi/10.2514/1.B35434},
doi = {10.2514/1.B35434},
number = {2},
urldate = {2024-07-22},
journal = {Journal of Propulsion and Power},
author = {Jang, Dongwook and Kwak, Youngchul and Kwon, Sejin},
month = mar,
year = {2015},
note = {Number: 2
Publisher: American Institute of Aeronautics and Astronautics},
keywords = {Bipropellant Thruster, Chamber Pressure, Convection Heat Transfer Coefficient, Coolant, Freestream, Kerosene, Mass Flow Rate, Stefan Boltzmann Constant},
pages = {761--765},
}
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