Dynamic Model Establishment of a Deployable Missile Control Fin with Nonlinear Hinge
Journal of spacecraft and rockets ; 42 , 1
2005
Aufsatz (Zeitschrift)
Unbekannt
Nonlinear Aeroelastic Analysis of a Deployable Missile Control Fin
Online Contents | 2004
|Toggle Hinge for Deployable Struts
NTRS | 1986
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