Flight Range Extension of a Guided Aerial Bomb with a Rocket Engine during Climb Bombing


  • I.S. Kravchuk Research & Development Company “Adron”, Kyiv, Ukraine
  • Bashynskyi Dmytro
  • V.V. Taranenko State Research Institute of Aviation, Kyiv, Ukraine
  • M.V. Zirka Researcher of the Central Research Institute of Armament and Military Equipment of Armed Forces of Ukraine, Kyiv




aircraft, climbing, guided aerial bomb, horizontal range, motion trajectory, solid-propellant rocket engine, total thrust impulse


The possibility of a significant flight range extension of a guided aerial bomb during climb bombing due to the jet thrust created by a solid-propellant rocket engine was considered. By means of simulation, a comparative analysis of the range of a guided aerial bomb equipped (not equipped) with a solid-propellant rocket engine under typical flight conditions of the carrier aircraft during level flight and climb bombing was performed. It was demonstrated that the use of a solid-propellant rocket engine, whose mass is 20 % of the guided aerial bomb’s mass, allows to increase the horizontal range of its flight at least twice.



FOMYCHEVA O.A. Improved Ballistic Capability of Guided Aerial Bombs. News of TulGU. Technical Sciences (in Russian). 2016, 4 , pp. 98-105. ISSN 2071-6168.

V.Y. KYRYLLOV. Bombing (in Russian). Moscow: Military Publishing, 1960.

SEMENOV S.S., V.N. KHARCHEV and A.Y. YOFFYN. Assessment of the Tech- nical Level of Weapons and Military Equipment (in Russian). Moscow: Radio and Communications, 2004. ISBN 978-5-256-01671-5.

AHAFONOV Y.M., O.M. ZHARYK, Y.M. OSYPOV and Y.A. TKACHENKO. The Ways of Aviation Munition Modernization Substantiation (in Russian). Systems of Arms and Military Equipment, 2017, 2 (50), pp. 50-52. ISSN 1997-9568.

VETROV V.V., V.A. DUNAEV, E.M. KOSTIANOI and V.V. MOROZOV Implementation of the Near-Zone Ballistic Efficiency Concept (in Russian). Basic Research, 2012, 11 (2), pp. 377-382. ISSN 1812-7339.

SEMENOV. S. Major R&D Activities to Improve Guided Aerial Bombs (in Russian). Foreign Military Review, 2016, 11 , pp. 63-67. ISSN 0134-921X.

KARPOV S.Y., YU.S. KUCHERENKO, YU.N. LEVCHENKO, et al. Controlled Aviation Bomb (in Russian). Patent RF No. RU2391624. Available from: http://www.freepatent.ru/patents/2391624

I.S. KRAVCHUK and V.V. TARANENKO. Realization of Proportional Self- Homing of the Corrected Aerial Bomb According to the Information of the Satellite Navigation System (in Ukrainian). Science and Technology of the Air Force of Ukraine, 2019, 3 (36), pp. 73-78. DOI 10.30748/nitps.2019.36.08.

ARKHANHELSKYI Y.Y., P.P. AFANASEV and E.H. BOLOTOV. Design of Surface-to-Air Guided Missiles (in Russian). Moscow: MAI, 2001. ISBN 978-5-7035-2335-4.

VASYLYN N.IA. and A.A. HURYNOVYCH. Air-Defence Systems (in Russian). Minsk: Popury, 2002. ISBN 978-985-438-681-2.

FYMUSHKYN F. and V.SLUHYN. Air-Defence Systems Short-Range “Pantir-C1-0 ˮ with Optoelectronic Guidance System (in Russian). M ilitary Parade Journal, 2004, 63 (03), pp 12-14. ISSN 1029-4678.






Research Paper


How to Cite

Flight Range Extension of a Guided Aerial Bomb with a Rocket Engine during Climb Bombing. (2021). Advances in Military Technology, 16(2), 265-276. https://doi.org/10.3849/aimt.01462

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