Theoretical and experimental research of supersonic missile ballistics

• Autorzy: Zygmunt B. , Motyl K. , Machowski B. , Makowski M. , Olejniczak E.

Identyfikatory

DOI

10.1515/bpasts-2015-0027

• Języki publikacji: EN

Abstrakty

EN

A mathematical-physical model of a supersonic missile was built, taking into account the mass and inertia properties. The model was implemented in the MathCAD14 simulation program. A numerical analysis of the missile ballistics was conducted and basic parameters were determined: range, altitude, velocity and acceleration, which enabled a test range program for manufactured missile models to be drawn up. Initial flight tests of missiles were carried out at the test range. Satisfactory accordance of experimental and theoretical dynamic parameters of the missile under study was obtained.

Słowa kluczowe

EN

missile exterior ballistics; mathematical model; computer simulation; test range experiment

PL

pociski balistyczne; model matematyczny; symulacja komputerowa

• Wydawca: Polska Akademia Nauk, Wydział IV Nauk Technicznych
• Czasopismo: Bulletin of the Polish Academy of Sciences. Technical Sciences
• Rocznik: 2015
• Tom: Vol. 63, nr 1
• Strony: 229--233
• Opis fizyczny: Bibliogr. 9, wykr., rys., tab., fot.

Twórcy

autor

Zygmunt B.

• Military University of Technology, 2 S. Kaliskiego St., 00-908 Warsaw, Poland

autor

Motyl K.

• Military University of Technology, 2 S. Kaliskiego St., 00-908 Warsaw, Poland

autor

Machowski B.

• Military University of Technology, 2 S. Kaliskiego St., 00-908 Warsaw, Poland

autor

Makowski M.

• Air Force Institute of Technology, 6 Ks. Boleslaw St., 01-494 Warsaw, Poland

autor

Olejniczak E.

• MESKO S.A., 122 Legionow St., 26-111 Skarzysko-Kamienna, Poland

Bibliografia

• [1] PRODAS, Arrow Tech Associates, Inc. USA (2008).
• [2] M. Martinez, N. Bruno, R. Kelly, and B. Sacco, Proc. 27th Intern. Symp. on Ballistics 1, 290-301 (2013).
• [3] S.D. Naik, “Stability criterion for a finned spinning projectile”, Def. Sci. J. 50 (1), 31-35 (2000).
• [4] J. Gacek, Modelling and Research of Dynamic Properties of Ballistic Objects), WAT, Warszawa, 1992, (in Polish).
• [5] B. Zygmunt and K. Motyl, “Computer assisted modelling of rocket flight using MathCad package”, Mechanik 7, 973-980 (2011).
• [6] L. Baranowski, “Equations of motion of a spin-stabilized projectile for flight stability testing”, J. Theor. Appl. Mech. 51 (1), 235-246 (2013).
• [7] L. Baranowski, “Numerical testing of flight stability of spinstabilized artillery projectiles”, J. Theor. Appl. Mech. 51 (2), 375-385 (2013).
• [8] L. Baranowski, “Effect of the mathematical model and integration step on the accuracy of the results of computation of artillery projectile flight parameters”, Bull. Pol. Ac.: Tech. 61 (2), 475-484 (2013).
• [9] MathCad, Mathsoft Engineering & Education, Inc. USA (2010).