A Unique Solution for Flight Body Angular Histories

Aerodynamic Characteristics of the Slotted Fin

Vol.I(76)EB23

Improved Aerodynamics for Configurations With Boattails

Development of a Projectile Penetration Theory. Report 1

ASimple Estimation Procedure for Roll Rate Derivatives

14vol2no1

Ballistic Missile Trajectory Prediction Using a State Transition Matrix

105mm_Mle57

Us 20120216697

6205x0825

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7) RAe_Cullis_Nov15

1-s2.0-S1270963813001375-main

07_3_NEW YORK_09-63_0083

171-A660

826070

645

1959 D149ZUNI 5.0 FFAR

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