Influence of Mass Parameters Modification on Manoeuvrability of 9K33 „OSA” Set 9M33M3 Missile

• Autorzy: Cichocki Maciej K. , Sokołowski Dariusz , Lewandowski Zbigniew

Identyfikatory

DOI

10.5604/01.3001.0014.3704

• Języki publikacji: EN

Abstrakty

EN

This paper discusses analytical method for realization of preliminary missile stability design calculations. Action has been taken to estimate influence of replacing massive blocks of analogue electronics with compact solutions of digital electronics in missiles remaining in operation. On an example of a short-range 9M33M3 missile from 9K33 „OSA” set and its previously analysed aerodynamic characteristics, the analysis of the centre of gravity location impact was carried out to determine maximum loads occurring in the two most interesting phases of flight: after booster engine burnout and directly after cruise engine burnout. The suggestion for modification suggestion of flight parameters’ optimization is presented which defines stability and its critical impact of these parameters on aeronautical engineering. For the tested missile, the methodology suggestions for the modification is discussed with the comparison of serially produced copies to define the ability of improving the flight parameters. The paper includes visualizations and quantity analysis of: maximal loads on the fuselage, minimal turn radius, and control wing inclination angle as missile’s angle of attack function.

Słowa kluczowe

EN

flight mechanics; short-range missile; missile stability

• Wydawca: Wojskowa Akademia Techniczna im. Jarosława Dąbrowskiego
• Czasopismo: Problemy Mechatroniki : uzbrojenie, lotnictwo, inżynieria bezpieczeństwa
• Rocznik: 2020
• Tom: Vol. 11, Nr 3 (41)
• Strony: 9--18
• Opis fizyczny: Bibliogr. 3 poz., tab., wykr.

Twórcy

autor

Cichocki Maciej K.

• Military Institute of Armament Technology, 7 Prymasa St. Wyszyńskiego Str., 05-220 Zielonka, Poland

autor

Sokołowski Dariusz

• Military Institute of Armament Technology, 7 Prymasa St. Wyszyńskiego Str., 05-220 Zielonka, Poland

autor

Lewandowski Zbigniew

• Military Institute of Armament Technology, 7 Prymasa St. Wyszyńskiego Str., 05-220 Zielonka, Poland

Bibliografia

• [1] Fleeman L. Eugene. 2001. Tactical Missile Design. Reston, VA, USA: American Institute of Aeronautics and Astronautics.
• [2] Perkins D. Courtland., Robert E. Hage. 1949. Airplane Performance Stability and Control. New York: John Wiley & Sons.
• [3] Chin S.S. 1961. Missile Configuration Design. New York, Orlando: McGraw-Hill Book Company Inc.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).