Abstract: The present disclosure relates to a powder of an austenitic alloy and a HIP:ed object manufactured thereof and a process for the manufacturing the HIP:ed object and its use in corrosive environments.

Abstract: The present disclosure relates to a powder of an austenitic alloy and a HIP:ed object manufactured thereof and a process for the manufacturing the HIP:ed object and its use in corrosive environments.

Abstract: 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.

Abstract: 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.

Abstract: A device for applying covering material provided in the form of a roll, said material having an adhesive layer (31) along one edge section. The device comprises a frame (1) with two parallel holders (3, 4) each for carrying a roll (5, 6) of covering material. A handle (7) connected to the frame extends transversely to said holders and inclined in relation to the plane of the holders. The device simultaneously receives oppositely wound rolls on the holders and permits a web of covering material to be fed from either of the two rolls in opposite directions, as desired. The handle (7) can be swung between two oppositely inclined positions so that the device can be moved in one or the other application direction as desired in order to feed out a web of covering material from the relevant roll of covering material. A web-shearing means (9, 10) is arranged on the frame for respective webs of covering material.