1. 1) Preclik, D., Hagemann, G., Knab, O., Brummer, L., Mäding, C., and Wiedmann, D.: LOX/Hydrocarbon Propellant Trade Considerations for Future Reusable Liquid Booster Engines, AIAA Paper 2005-3567, 2005.
2. 2) Burkardt, H., Sippel, M., Herbertz, A., and Klevanski, J.: Kerosene vs Methane: A Propellant Tradeoff for Reusable Liquid Booster, J. Spacecraft and Rockets, 41(2004), pp. 762-769.
3. 3) Locke, J., Pal, S., and Woodward, R.: Chamber Wall Heat Flux Measurements for a LOX/CH4 Propellant Uni-Element Rocket, AIAA Paper 2007-5547, 2007.
4. 4) Ishikawa, Y., Kodama, S., Ishii, M., Higashino, K., Ikeda, H., Arita, M., Arita, G. P., and Mossolov, S. V.: LOX /LNG Engine Design and Test Results for J-II Rocket, AIAA Paper 2000-3454, 2000.
5. 5) Sun, J.: An Experimental Study of LOX/Methane Subscale Injector, IAC, 65th International Astronautical Congress, Canada, IAC-14.C4.3.10, 2014.