Dynamic Model Establishment of a Deployable Missile Control Fin with Nonlinear Hinge
Dae-Kwan Kim, Jae-Sung Bae, In Lee, Jae-Hung Han
Journal of Spacecraft and Rockets ; 42 , 1 ; 66-77
2005-01-01
12 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Dynamic Model Establishment of a Deployable Missile Control Fin with Nonlinear Hinge
Online Contents | 2005
|Nonlinear Aeroelastic Analysis of a Deployable Missile Control Fin
Online Contents | 2004
|Toggle Hinge for Deployable Struts
NTRS | 1986
|