Browse > Article
http://dx.doi.org/10.5139/JKSAS.2015.43.5.456

Technology Review and Development Trends of Dual-Bell Nozzle for Altitude Compensation  

Choi, Junsub (Department of Aerospace Engineering, Graduate School at Chungnam National University)
Huh, Hwanil (Department of Aerospace Engineering, Chungnam National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.43, no.5, 2015 , pp. 456-465 More about this Journal
Abstract
Dual-bell nozzle can overcome the performance losses of the conventional bell-shaped nozzles which induced by off-design operations with either over-expanded or under-expanded exhaust flow and minimize the losses of the specific impulse. In United States, Rocketdyne analyzed thrust characteristics according to the shape of the expansion nozzle and NASA conducted hot firing tests with various altitudes. DLR, which is one of the research institute of the Europe, is carrying out research for the different cases of inflection angle, nozzle length and expansion ratio. MAI of Russia applied the slot nozzle to the expansion region in order to reduce the performance losses. In Asia, both the Japan and the India are researching on the dual-bell nozzle and Mitsubishi cooperation of the Japan registered its patent. In this paper, concepts and performance of dual-bell nozzle, which can compensate altitude, are investigated and trends of current research are summarized. It is necessary for Korea to research on the dual-bell nozzle for lucrative space development.
Keywords
Dual-Bell Nozzle; Altitude Compensation; Expansion Ratio; Technology Review;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Genin, C., Stark, R., Haidn, O., Quering, K. and Frey, M., Experimental and numerical study of dual bell nozzle flow, Progress in Flight Physics, Vol. 5, Torus Press, Moscow, 2013, pp.363-376.
2 Hagemann, G., Immich, H., Nguyen, T. V. and Dumnov, G. E., "Advanced roket nozzle", Journal of Propulsion and Power, Vol. 14, No. 5, 1998, pp.620-634.   DOI
3 Gopalapillai, R. and Kim, H. D., "A CFD study on the Supersonic Flow through a Dual Bell Nozzle", KSPE Spring Conference, 2012, pp.324-330.
4 Nasuti, F., Onofri, M., and Martelli, E., "Effect of Wall Shape and Real Gas properties on Dual bell nozzle flow field", AIAA 2005-3943, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July, 2005.
5 JP-P-2008-00069502, "Rocket Nozzle and Control Method for Combustion Gas Flow in Rocket Engine", Patent, Japan, 2008.
6 Manski, D., Goertz, C., SaBnick, H., Hulka, J. R., Goracke, B. D. and Levack, D., "Cycles for Earth-to-Orbit Propulsion", Journal of Propulsion and Power, Vol. 14, No. 5, 1988, pp.588-604.   DOI
7 Kwon, M. C. and Semenov, V. V., "Thrust Characteristics of Slot Nozzle with Dual-Bell Contour", KSPE Fall Conference, 2014, pp.562-565.
8 Kim, H. D. and Koo, B. S., "A Study of The Flow Charateristics through a Supersonic Dual Bell Nozzle", Journal of the Korean Society of Propulsion Engineers, Vol. 4, No. 4, 2000, pp.70-77.
9 Davis, K., Fortner, E., Heard, M., McCallum, H. and Putzke, H., "Experimental and computational investigation of a dual bell nozzle", 53rd AIAA Aerospace Sciences Meeting, January, 2015.
10 Horn, M. and Fisher, S., "Dual-Bell altitude compensating nozzle", 5th Annual Propulsion Engineering Research Center Symposium, September, 1993, pp.140-147.
11 Collins, J., Hurlbert, E., Romig, K. and Melcher, J., "Sea-level flight demonstration & altitude characterization of a LO2/LCH4 based accent propulsion lander", JSC-CN-18506, 2009.
12 Daniel S. and Trong T., "Proposed Flight Research of a Dual-Bell Rocket Nozzle Using the NASA F-15 Airplane", AIAA Journal, 2013.
13 Immuch, H. and Caporicci, M., "Status of the FESTIP rocket propulsion technology programme", AIAA Journal, 1997.
14 Genin, C., Gernoth, A. and Stark, R., "Experimental and numerical study of heat flux in dual bell nozzles", AIAA Journal, 2011.
15 Genin, C. and Stark, R., "Experimental study of dual bell nozzles", 2nd European Conference for Aerospace Sciences, 2007.
16 Reijasse, P., Coponet, D., Luyssen, J., Bar, V., Palerm, S., Oswald, J., Amouroux, F., Robinet, J. and Kuszla, P., "Wall pressure and thrust of a dual bell nozzle in a cold gas facility", Progress in Propulsion Physics, Vol. 2, Torus Press, Moscow, 2011, pp.655-674.
17 Semenov, V. V., Shevtsov, V., "The Rocket Engine Jet Nozzle with High-Altitude Characteristics", ISTC Project Final Technical Report, 2008.
18 Semenov, V. V., Finogenov, S. L., Ivanov, I. E., Krykov, I. A., Talalayev, A. A., "Liquid Propulsion with Altitude Compensation Concept Trade Study", 57th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics and the International Institute of Space Law, Valencia, Spain, 2006.
19 Kimura, T. and Niu, K., "Experimental and analytical study for design of dual-bell nozzles", 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July, 2009.
20 Narayan, A. and Panneerselvam, S., "Study of the effect of over-expansion factor on the flow transition in dual bell nozzles", World Academy of Science, Engineering and Technology, vol. 6, No. 8, 2012, pp.1304-1308.