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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2020
/
Article
/
Tab 1
/
Research Article
Flight Stability of Canard-Guided Dual-Spin Projectiles with Angular Rate Loops
Table 1
Parameters of the 155 mm dual-spin projectile.
Parameter
Value
Parameters
Value
42.8
1.893
0.155
0.01887
450
1450
3.6
13.2
3.6
0.7