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http://dx.doi.org/10.6108/KSPE.2017.21.2.060

Comparison of the Mission Performance of Korean GEO Launch Vehicles for Several Propulsion Options  

Hong, Mir (Department of Aerospace Engineering, Pusan National University)
Yang, Seong-Min (Department of Aerospace Engineering, Pusan National University)
Kim, Hye-Sung (Department of Aerospace Engineering, Pusan National University)
Yoon, Youngbin (Department of Mechanical and Aerospace Engineering, Seoul National University)
Choi, Jeong-Yeol (Department of Aerospace Engineering, Pusan National University)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.21, no.2, 2017 , pp. 60-71 More about this Journal
Abstract
A trajectory analysis program is developed using a 3DOF trajectory model for the performance analysis of geostationary launch vehicles by system options. Launch trajectory and the performance of injection at GTO was estimated using this program for several propellant options, engine types, number of engines and the location of launch site. Results of the analysis presents that the possibility of mission accomplishment by several design options using domestic launch sites and the development direction of GEO launch vehicles.
Keywords
Space Launch Vehicle; Mission Design; Geostationary Earth Orbit(GEO); Geostationary Transfer Orbit(GTO);
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
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