EP 0335761 B1 19930120 - AIRBORNE VEHICLE WITH AT LEAST ONE RELEASABLE PROPULSION UNIT
Title (en)
AIRBORNE VEHICLE WITH AT LEAST ONE RELEASABLE PROPULSION UNIT
Publication
Application
Priority
FR 8804213 A 19880330
Abstract (en)
[origin: EP0335761A1] - Airborne vehicle (1) comprising at least one temporary releasable propulsion unit (2) connected to the rest (3) of said vehicle by means of a fit (4, 7-5,8-9, 10) capable of allowing said propulsion unit to slide parallel to its axis in the opposite direction to the rest (3) of the vehicle. <??>- According to the invention, this vehicle is notable in that communication (17) is established between, on the one hand, the space (16) located within said fit and arranged between the front of said propulsion unit and said rest (3) of the vehicle and, on the other hand, the aerodynamic flow around said vehicle (1). <??>- The natural separation of said propulsion unit (2) from the rest (3) of said missile (1). <IMAGE>
IPC 1-7
IPC 8 full level
B64G 1/64 (2006.01); F42B 15/36 (2006.01)
CPC (source: EP US)
F42B 15/36 (2013.01 - EP US)
Designated contracting state (EPC)
BE CH DE ES GB IT LI NL SE
DOCDB simple family (publication)
EP 0335761 A1 19891004; EP 0335761 B1 19930120; CA 1332537 C 19941018; DE 68904453 D1 19930304; DE 68904453 T2 19930603; ES 2037972 T3 19930701; FR 2629583 A1 19891006; FR 2629583 B1 19930618; JP 2954948 B2 19990927; JP H0210100 A 19900112; US 4903605 A 19900227
DOCDB simple family (application)
EP 89400663 A 19890309; CA 595123 A 19890330; DE 68904453 T 19890309; ES 89400663 T 19890309; FR 8804213 A 19880330; JP 6943589 A 19890323; US 32290289 A 19890314