Keywords and phrases: bipropellant liquid rocket engines, combustion chamber temperature.
Received: August 18, 2021; Accepted: September 24, 2021; Published: December 8, 2021
How to cite this article: Nevsan Sengil, Theoretical investigation of rocket engines for oxygen and ethane liquid bipropellant, JP Journal of Heat and Mass Transfer 24(2) (2021), 309-320. DOI: 10.17654/0973576321006
This Open Access Article is Licensed under Creative Commons Attribution 4.0 International License
References:
[1] R. J. Cassady, R. H. Frisbee, J. H. Gilland, M. G. Houts, M. R. LaPointe, C. M. Maresse-Reading, S. R. Oleson, J. E. Polk, D. Russell and A. Sengupta, Recent advances in nuclear powered electric propulsion for space exploration, Energy Conversion and Management 49(3) (2008), 412-435. [2] S. K. Pradhan, V. Kedia and P. Kour, Review on different materials and their characterization as rocket propellant, Materials Today: Proceedings 33(8) (2020), 5269-5272. [3] A. Davenas and J. Thépenier, Recent progress in the prediction and analysis of the operation of solid rocket motors, Acta Astronautica 44(7-12) (1999), 461-469. [4] G. Cai, J. Fang, X. Xu and M. Liu, Performance prediction and optimization for liquid rocket engine nozzle, Aerospace Science and Technology 11(2-3) (2007), 155-162. [5] M. Gieras and A. Gorgeri, Numerical modelling of the hybrid rocket engine performance, Propulsion and Power Research 10(1) (2021), 15-22. [6] Y. K. Ponraj and B. Borah, Separation of methane from ethane and propane by selective adsorption and diffusion in MOF Cu-BTC: A molecular simulation study, Journal of Molecular Graphics and Modelling 97 (2020), 107574. [7] G. A. Bird, Molecular Gas Dynamics, and the Direct Simulation of Gas Flows, Clarendon, Oxford, 1994. [8] G. P. Sutton and O. Biblarz, Rocket Propulsion Elements, Wiley, Hoboken, New Jersey, USA, 2017. [9] I. Glassman and R. A. Yetter, Combustion, Elsevier Academic Press, Burlington, MA, USA, 2008. [10] D. G. Goodwin, R. L. Speth, H. K. Moffat and B. W. Weber, Cantera: An object-oriented software toolkit for chemical kinetics, thermodynamics, and transport processes. https://www.cantera.org, 2021, Version 2.5.1. doi: 10.5281/zenodo.4527812. [11] R. V. Mykhalchyshyn, M. S. Brezgin and D. A. Lomskyi, Methane, kerosene and hydrogen comparative as a rocket fuel for launch vehicle pneumohydraulic supply system development, Space Science and Technology 24(2) (2018), 12-17.
|