초록 ▼

A missile launching system including a launch rail for attachment to an aircraft and having a longitudinal slot, and at least two hangers for attachment to the missile at longitudinally spaced locations thereof and having a cross-section configured to be received in the longitudinal slot in the laun

A missile launching system including a launch rail for attachment to an aircraft and having a longitudinal slot, and at least two hangers for attachment to the missile at longitudinally spaced locations thereof and having a cross-section configured to be received in the longitudinal slot in the launch rail. The rearmost hanger includes two separable main parts, including a first main part for engagement with a respective lateral, first groove section of the slot, and a second main part configured to be attached to the missile and be slidably guided in a second groove section of the slot normal to the first groove section and opening towards the missile. The second main part includes laterally extending collars configured to interact in close proximity with respective rail sections facing the missile. The second main part is configured to separate from the first part when launching the missile.

대표청구항 ▼

The invention claimed is: 1. A missile launching system, comprising:a launch rail configured to be attached to an aircraft, the launch rail comprising a substantially T-shaped longitudinal slot, andat least two hanger members configured to be attached to a missile at longitudinally spaced locations,

The invention claimed is: 1. A missile launching system, comprising:a launch rail configured to be attached to an aircraft, the launch rail comprising a substantially T-shaped longitudinal slot, andat least two hanger members configured to be attached to a missile at longitudinally spaced locations, at least a rearmost hanger member of the at least two hanger member comprising a substantially T-shaped section configured to be received in the substantially T-shaped longitudinal slot in the launch rail,wherein the rearmost hanger member comprises two separable main parts, the two separable main parts comprising a first main part configured to engage a respective lateral, first groove section of the substantially T-shaped longitudinal slot, and a second main part configured to be attached to the missile and be slidably guided in a second groove section of the substantially T-shaped longitudinal slot normal to the first groove section and opening towards the missile, said second main part comprising laterally extending collars configured to interact in close proximity with respective rail sections facing the missile, said second main part being configured to separate from the first part when launching the missile.