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Implementation of MPMM ballistic model for calculation of differential coefficients for TFTs according to NATO STANAG 4119 1

Ivan Katalinić


Full text: english pdf 1.406 Kb

page 169-196

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Full text: croatian pdf 1.103 Kb

page 141-168

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Abstract

MPMM ballistic model (modified point mass model) is used to calculate all necessary ballistic trajectory elements (range, time of flight, angle of fall, maximum ordinate, differential coefficients, etc.) for classical spin-stabilized artillery projectiles. In this paper, differential and algebraic equations that fully define MPMM ballistic model and its program solution (MPMM_D30) are presented. The MPMM_D30 enables calculation of differential coefficients for H122mmD30 howitzer (and other ballistic trajectory elements) that are an integral part of TFTs according to NATO STANAG2 4119 (Adoption of a Standard Cannon Artillery Firing Table Format, Brussels, 2007), which should become HRVN STANAG3 4119.

Keywords

external ballistics; ballistic model; standard atmosphere; projectile trajectory; meteorological report; differential equations; H122mmD30

Hrčak ID:

261157

URI

https://hrcak.srce.hr/261157

Publication date:

30.6.2021.

Article data in other languages: croatian

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