EP 0078921 B1 19870527 - TAIL UNIT WITH REDUCED GROUND WIND SENSITIVITY
Title (en)
TAIL UNIT WITH REDUCED GROUND WIND SENSITIVITY
Publication
Application
Priority
DE 3144073 A 19811106
Abstract (en)
[origin: EP0078921A2] 1. Fixed or hinged tail unit for guided or unguided supersonic missile, characterised in that the fins (2) of the tail unit are formed for reducing their effectiveness at the beginning of the flight phase so that a reinforced pressure equalisation between their upper and lower sides is possible by the fins (2) exhibiting a small elongation, in particular an elongation less than 1, and/or the fins (2) being provided externally of the contour of the flight body in the region of their end directed to the flight body with perforations, slits (5, 6, 6') or the like extending in the longitudinal direction.
IPC 1-7
IPC 8 full level
F42B 10/06 (2006.01); F42B 10/14 (2006.01)
CPC (source: EP)
F42B 10/06 (2013.01); F42B 10/14 (2013.01)
Citation (examination)
DE 2045687 A1 19720323 - DYNAMIT NOBEL AG
Designated contracting state (EPC)
BE DE FR GB IT SE
DOCDB simple family (publication)
EP 0078921 A2 19830518; EP 0078921 A3 19840606; EP 0078921 B1 19870527; DE 3144073 A1 19830519; DE 3276446 D1 19870702; MX 163263 B 19920330
DOCDB simple family (application)
EP 82109279 A 19821007; DE 3144073 A 19811106; DE 3276446 T 19821007; MX 19503882 A 19821103