Résultats Préliminaires de l’Étude des Configurations HEMi

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Authors
  1. Lestage, R.
Corporate Authors
Defence R&D Canada - Valcartier, Valcartier QUE (CAN)
Abstract
For the HEMi-TD project, the first step was to do a comparative study of several missile configurations. These comparisons have been performed for different combinations of airframe weight and aerodynamics properties. For each case, different requirements for range and speed have been studied. It is proposed to further investigate the performance of the configurations composed of a two-stage missile where a booster accelerates a dart that separates from the booster and continues its trajectory without sustained propulsion.

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Keywords
Missile;Hypersonics;Parametric study;Comparative study;HEMi (High Energy Missile);Aerodynamic coefficients;Kinetic energy penetrators
Report Number
DRDC-VALCARTIER-TN-2003-199 — Technical Note
Date of publication
01 Sep 2004
Number of Pages
1481
DSTKIM No
CA024998
CANDIS No
522518
Format(s):
CD ROM

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