EP 0064433 B1 19860219 - GUIDED MISSILE
Title (en)
GUIDED MISSILE
Publication
Application
Priority
FR 8107916 A 19810421
Abstract (en)
[origin: US4441670A] A guided projectile comprising an energy source supplying a gas flow which feeds two pairs of exhaust nozzles, each pair of nozzles being disposed in the corresponding steering plane. Each of these nozzles is provided with a valve for regulating the relative flowrates of the throughflowing gases; this valve being formed essentially by a pivoting vane hinged about an axis; these vanes are interlocked in pairs and positioned by means of two independent mechanisms formed by a deformable parallelogram, the element 40 being the drive element. According to the invention, the directions of the thrust forces created by the nozzles converge at a point P situated on the axis of the projectile and this point P may merge with the center of gravity G of the projectile.
IPC 1-7
IPC 8 full level
F02K 9/90 (2006.01); B64C 15/02 (2006.01); B64G 1/00 (2006.01); F02K 9/08 (2006.01); F41G 7/00 (2006.01); F42B 15/00 (2006.01); G05D 1/10 (2006.01)
CPC (source: EP US)
F42B 10/663 (2013.01 - EP US)
Designated contracting state (EPC)
AT BE CH DE GB IT LI NL SE
DOCDB simple family (publication)
EP 0064433 A1 19821110; EP 0064433 B1 19860219; AT E18096 T1 19860315; CA 1185479 A 19850416; DE 3269123 D1 19860327; FR 2504252 A1 19821022; FR 2504252 B1 19870306; JP S57181953 A 19821109; US 4441670 A 19840410
DOCDB simple family (application)
EP 82400634 A 19820406; AT 82400634 T 19820406; CA 401311 A 19820420; DE 3269123 T 19820406; FR 8107916 A 19810421; JP 6411782 A 19820419; US 37025582 A 19820420