Global Patent Index - EP 1286129 B8

EP 1286129 B8 20071031 - Incendiary munition for a flight stabilised penetrating projectile

Title (en)

Incendiary munition for a flight stabilised penetrating projectile

Title (de)

Brandsatz für ein flügelstabilisiertes Wuchtgeschoss

Title (fr)

Munition incendiaire pour un projectile pénétrant stabilisé par empennage

Publication

EP 1286129 B8 20071031 (DE)

Application

EP 02012954 A 20020612

Priority

DE 10140600 A 20010818

Abstract (en)

[origin: EP1286129A1] An incendiary composition (14) comprises titanium sponge (in wt.%) (85-96) and an epoxide resin or a polyester resin (4-15), and has a density of 1.7-2.8 g/cm3. The incendiary composition is provided in a tail region (8) of a fin-stabilized kinetic energy projectile, and upon impact with a target (13), enters the target as a separate unit behind the penetrator (2) of the projectile.

[origin: EP1286129A1] An incendiary composition (14) comprises titanium sponge (in wt.%) (85-96) and an epoxide resin or a polyester resin (4-15), and has a density of 1.7-2.8 g/cm<3>. The incendiary composition is provided in a tail region (8) of a fin-stabilized kinetic energy projectile, and upon impact with a target (13), enters the target as a separate unit behind the penetrator (2) of the projectile.

IPC 8 full level

F42B 12/44 (2006.01); C06B 45/00 (2006.01); C06C 15/00 (2006.01)

CPC (source: EP)

C06B 45/00 (2013.01); C06C 15/00 (2013.01)

Designated contracting state (EPC)

DE FR GB

DOCDB simple family (publication)

EP 1286129 A1 20030226; EP 1286129 B1 20070926; EP 1286129 B8 20071031; DE 10140600 A1 20030306; DE 50210961 D1 20071108; IL 151292 A 20061005; IL 151292 D0 20030410; US 2003034102 A1 20030220; US 2005230016 A1 20051020; US 6849140 B2 20050201

DOCDB simple family (application)

EP 02012954 A 20020612; DE 10140600 A 20010818; DE 50210961 T 20020612; IL 15129202 A 20020815; US 22287202 A 20020819; US 3396505 A 20050113