Abstract: A deployable device mountable on a carrier vehicle and configured to collect situation awareness data. The deployable device includes at least one recorder device configured to collect situation awareness data. The deployable device is capable of being ejected from the carrier vehicle and can be configured to operate as a vehicle and/or be towed by the carrier vehicle. The deployable device can continue collection of situation awareness data after being ejected.

Abstract: A deployable device mountable on a carrier vehicle and configured to collect situation awareness data. The deployable device includes at least one recorder device configured to collect situation awareness data. The deployable device is capable of being ejected from the carrier vehicle and can be configured to operate as a vehicle and/or be towed by the carrier vehicle. The deployable device can continue collection of situation awareness data after being ejected.

Abstract: A deployable device mountable on a carrier vehicle and configured to collect situation awareness data. The deployable device includes at least one recorder device configured to collect situation awareness data. The deployable device is capable of being ejected from the carrier vehicle and can be configured to operate as a vehicle and/or be towed by the carrier vehicle. The deployable device can continue collection of situation awareness data after being ejected.

Abstract: A deployable device mountable on a carrier vehicle and configured to collect situation awareness data. The deployable device includes at least one recorder device configured to collect situation awareness data. The deployable device is capable of being ejected from the carrier vehicle and can be configured to operate as a vehicle and/or be towed by the carrier vehicle. The deployable device can continue collection of situation awareness data after being ejected.

Abstract: A method of constructing a panel for an aircraft subassembly is provided. The panel has interior and exterior sides relative to the subassembly and comprises a skin and a support structure. The support structure comprises a plurality of longerons and frames constituting support-structure elements and arranged substantially in a grid, and projecting substantially transversely from the skin toward the interior side. The method comprises providing a flat sheet of structural material, wherein the sheet comprises one or more cutouts, and forming the support structure by folding the sheet, wherein the longerons and frames are formed from overfolded areas of the sheet adjacent the cutouts, and wherein non-overfolded areas of the sheet constitute the skin.

Abstract: A system and method for shedding redundant launcher tank mass, comprising progressing means, and cutting means configured to cut redundant propellant tank wall, the system configured to progress inside the tank, along the tank wall in an initially predetermined rate.

Abstract: A system and method for shedding redundant launcher tank mass, comprising progressing means, and cutting means configured to cut redundant propellant tank wall, the system configured to progress inside the tank, along the tank wall in an initially predetermined rate.

Abstract: The present invention relates to a device for the stabilization of teeth, in particular molar teeth having a cavity which comprises a screw provided with an outer thread and means at its outer end for holding it and a hollow nut provided with an inner thread adapted to the outer thread of the screw and means at the outer end of the nut for holding it. The present invention also relates to a method for the treatment of a tooth having a cavity with the aid of said device.