EP 0737297 B1 19971008 - MISSILE LAUNCHING AND STEERING SYSTEM
Title (en)
MISSILE LAUNCHING AND STEERING SYSTEM
Title (de)
ABSCHLUSSVORRICHTUNG UND MIT EINER LENKVORRICHTUNG VERSEHENE RAKETE
Title (fr)
SYSTEME DE LANCEMENT ET D'ORIENTATION D'ENGINS VOLANTS
Publication
Application
Priority
- FR 9501423 W 19951027
- RU 94040077 A 19941027
- RU 95110350 A 19950703
Abstract (en)
[origin: WO9613694A1] A launching system, particularly a missile launching and steering system, whereby angle-launched missiles may be modernised by converting them into controlled missiles for circular defence, and ejection of the passive mass on the launch pad is prevented. For this purpose, the launching system includes a driven launching means (10) for the aerodynamic control surfaces (2) and a steering means comprising at least one gas generator (4) and nozzles (5) joined thereto. The steering means consists of an annular body (3) rigidly connected to the rear portion of the missile body. The inner surface of the annular body is tapered and covered with a thermal insulating material to form a gas ducting (7) with a profile in line with that of the sustainer motor nozzle (6) of the missile.
IPC 1-7
IPC 8 full level
F41F 3/04 (2006.01); F41F 3/077 (2006.01); F42B 10/66 (2006.01); F42B 15/00 (2006.01)
CPC (source: EP US)
F41F 3/04 (2013.01 - EP US); F41F 3/077 (2013.01 - EP US); F42B 10/66 (2013.01 - EP US); F42B 10/663 (2013.01 - EP US)
Designated contracting state (EPC)
CH DE DK ES FR GB IT LI NL SE
DOCDB simple family (publication)
WO 9613694 A1 19960509; AU 3848195 A 19960523; AU 708097 B2 19990729; DE 69500842 D1 19971113; DE 69500842 T2 19980226; DK 0737297 T3 19971222; EP 0737297 A1 19961016; EP 0737297 B1 19971008; ES 2107921 T3 19971201; FI 111032 B 20030515; FI 962638 A0 19960626; FI 962638 A 19960823; IL 115749 A0 19960119; IL 115749 A 20000229; JP 3692537 B2 20050907; JP H09507567 A 19970729; KR 100404037 B1 20040324; NO 310637 B1 20010730; NO 962653 D0 19960621; NO 962653 L 19960827; TW 319825 B 19971111; UA 27153 C2 20000228; US 5823469 A 19981020
DOCDB simple family (application)
FR 9501423 W 19951027; AU 3848195 A 19951027; DE 69500842 T 19951027; DK 95936617 T 19951027; EP 95936617 A 19951027; ES 95936617 T 19951027; FI 962638 A 19960626; IL 11574995 A 19951024; JP 51436396 A 19951027; KR 19960703453 A 19960627; NO 962653 A 19960621; TW 85100345 A 19960112; UA 96072972 A 19951027; US 66330896 A 19960626