2015
DOI: 10.1515/bpasts-2015-0027
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Theoretical and experimental research of supersonic missile ballistics

Abstract: Abstract.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 exp… Show more

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Cited by 9 publications
(7 citation statements)
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“…2). The test missile is a second stage of the missile discussed in the paper (Zygmunt et al, 2015) and it is stabilised in banking angle. The starting engine enables to achieve the speed of 950 m/s in the boost phase.…”
Section: Results Of Numerical Calculations and Final Conclusionmentioning
confidence: 99%
“…2). The test missile is a second stage of the missile discussed in the paper (Zygmunt et al, 2015) and it is stabilised in banking angle. The starting engine enables to achieve the speed of 950 m/s in the boost phase.…”
Section: Results Of Numerical Calculations and Final Conclusionmentioning
confidence: 99%
“…the air-path inclination angle and χ a is the azimuth angle of v, i.e. the air-path azimuth angle 7 . Also let us stress that if we use a 3-vector column notation we write the coordinates in the order x, y, z starting from the top, this again is merely a convention.…”
Section: Phase Space Reference Frame: Air-flow Reference Systemmentioning
confidence: 99%
“…(29c) 7 In fact, the choice of axes is unimportant to this work, sometimes literature chooses a version where the z-axis points down and the y-axis points to the right. We find an upward z-axis more natural but as said -it does not influence the derivation.…”
Section: Derivation Of the M-model Let Us Recall Thatmentioning
confidence: 99%
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“…The operation of a solid propellant rocket engine of a newly-developed Polish two-stage, anti-aircraft supersonic missile [10,11] is the subject of the analysis in this paper. Starting from the required missile performance, this paper presents a physical model of the solid propellant charge of a complex (atypical) shape, a mathematical model of the rocket engine operation (in terms of thermodynamics), and computer simulations on the basis of the original SRMIB (solid rocket motor internal ballistics) software.…”
Section: Introductionmentioning
confidence: 99%