EP 0238717 B1 19900801 - STEERABLE MISSILE
Title (en)
STEERABLE MISSILE
Publication
Application
Priority
DE 3606423 A 19860227
Abstract (en)
1. Controllable missile (FK) including control elements (4, 23, 33, 34, 44, 44', R1, 71, 91, 101) to influence the flight path of the missile, with a rotor which rotates relative to the remaining missile body, and a console (A) on which are arranged the control elements which are adjustable so as to influence the flight path of the missile with the aid of a control member (C, 45, 46, K, 92, 104), characterised in that the rotor has its propelling rotary drive (4, 22, 23, 44, R1, 71, 01, 101), that a further control member (E) to influence the rotatation of the rotor is provided between the rotor and the remaining missile body, and that said further control member (E) includes means which actuate the control member (C, 45, 46, K, 92, 104) for the control elements on the console.
IPC 1-7
IPC 8 full level
F42B 10/64 (2006.01)
CPC (source: EP US)
F42B 10/64 (2013.01 - EP US)
Designated contracting state (EPC)
CH FR GB IT LI SE
DOCDB simple family (publication)
DE 3606423 A1 19870903; DE 3645077 C2 19960627; EP 0238717 A1 19870930; EP 0238717 B1 19900801; US 4927096 A 19900522; US 5065957 A 19911119; US 5083724 A 19920128
DOCDB simple family (application)
DE 3606423 A 19860227; DE 3645077 A 19860227; EP 86115867 A 19861114; US 1688187 A 19870220; US 51629090 A 19900430; US 51651690 A 19900430