Global Patent Index - EP 2433084 A2

EP 2433084 A2 20120328 - GUIDED MISSILE

Title (en)

GUIDED MISSILE

Title (de)

LENKFLUGKÖRPER

Title (fr)

MISSILE GUIDÉ

Publication

EP 2433084 A2 20120328 (EN)

Application

EP 10784603 A 20100518

Priority

  • US 2010035178 W 20100518
  • US 17939109 P 20090519

Abstract (en)

[origin: WO2011019424A2] A missile (10) comprising a projectile body (20), a payload (60) contained within the nose portion (30), wings (70) stowed within the mid portion (40), and fins (80) stored within the tail portion (50). The wings (70) can be deployed during intermediate stages of the flight path when lift is advantageous, and re-stowed during terminal stages when an almost vertical angle-of-attack is desired. The fins (80) function as stabilizing components during the early ballistic stage of the flight path and function as guiding components thereafter.

IPC 8 full level

F42B 10/64 (2006.01); F42B 10/14 (2006.01)

CPC (source: EP US)

F42B 10/14 (2013.01 - EP US); F42B 10/64 (2013.01 - EP US)

Citation (search report)

See references of WO 2011019424A2

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

DOCDB simple family (publication)

WO 2011019424 A2 20110217; WO 2011019424 A3 20110505; EP 2433084 A2 20120328; EP 2433084 B1 20130508; US 2012068002 A1 20120322

DOCDB simple family (application)

US 2010035178 W 20100518; EP 10784603 A 20100518; US 78186810 A 20100518