JOURNAL BROWSE
Search
Advanced SearchSearch Tips
Analysis of Flight Trajectory Characteristics of the MRBM by Adjusting the Angle of a Flight Path
facebook(new window)  Pirnt(new window) E-mail(new window) Excel Download
 Title & Authors
Analysis of Flight Trajectory Characteristics of the MRBM by Adjusting the Angle of a Flight Path
Kim, Jiwon; Kwon, Yong Soo;
  PDF(new window)
 Abstract
North Korea has developed ballistic missiles over the past 30 years. It is believed that they have a variety of ballistic missiles more than 1,000. Because these ballistic missiles threaten South Korea directly, accurate analysis of them is essential. Flight trajectories of the ballistic missiles are generally changed by means of adjusting payload weight, Isp, flight path angle, and cut-off time. The flight path angle is widely used to control the missile range. However it is difficult to predict the missile trajectory exactly in real operational environment because the missile could be launched according to its intention and purpose. This work analyzed the 1,000 km range MRBM's trajectory characteristics from adjusting flight path angle which is depressed as well as lofted method. The analysis of missile trajectory characteristics is based on the simulation of the missile trajectory model developed by KNDU research team.
 Keywords
Medium Range Ballistic Missile;Ballistic Missile Defense;Flight Path Angel;
 Language
Korean
 Cited by
1.
잠수함 발사 탄도미사일 탐지를 위한 해상 센서플랫폼의 배치에 관한 연구,김지원;권용수;김남기;김동민;박영한;

한국항행학회논문지, 2015. vol.19. 5, pp.363-369 crossref(new window)
 References
1.
H. Kim, K. Kim, G. Jeon, "A Requirement Assessment Algorithm for Anti-Ballistic Missile Considering Ballistic Missile's Flight Characteristics," Journal of the Korea Institute of Military Science and Technology, Vol. 14, No. 6, pp. 1009-1017, 2011. crossref(new window)

2.
H. Kwon, B. Lee, Y. Kim, K. Choi, "An Effectiveness Analysis of Anti-Ballistic Missile Launcher Arrangement for the Lower Tier Defense Against the Ballistic Missile," Journal of the Korea Institute of Military Science and Technology, Vol. 16, No. 5, pp. 590-597, 2013. crossref(new window)

3.
Y. Kwon, B. Choi, "Analysis of the Flight Trajectory Characteristics of Ballistic Missiles," Journal of the Misitary Operations Research Society of Korea, Vol. 32, No. 1, pp. 176-187, 2006.

4.
Y. Kwon, "Technical Analysis and Assessment of North Korean Ballistic Missiles," Journal of National Defense Studies Vol. 56, No. 1, pp. 9-10, 2013.

5.
W. Lee, "Ballistic Missile and Space Launch Vehicle of the World," Agency for Defense Development, p. 69, 2004.

6.
Francis J. Hale, "Introduction to Space Flight," Prentice Hall, pp. 280-288, 1994.

7.
Y. Kwon, J. Kim, K. Lee, "The Derivation of System Required Capabilities for the Successful Conduct of the Lower Tier BMD," Journal of the Misitary Operations Research Society of Korea, Vol. 37, No. 2, pp. 12-15, 2011.

8.
J. Ahn, Y. Kwon, "Analysis of the Flight Trajectory Characteristics of Ballistic Missiles Depending on the Operational Parameters," Korea Association of Defense Industry Studies, Vol. 20, No. 2, pp. 119-136, 2013.

9.
D. Wright, T. Kadyshev, "An Analysis of the North Korean Nodong Missile," Science and Global Security, Vol. 4, pp. 129-160, 1994

10.
Jane's Strategic Weapon Systems, "'Scud-C' Variant (Hwasong 6), 'Scud D' Variant(Hwasong 7, and 'Scud-ER')," 2012. 9.

11.
Jane's Strategic Weapon System, "Ballistic missile Technologies and Performance Analysis," 2013. 11. 15.