Abstract: An injection apparatus (2) comprising a housing (4) and an injector sub-assembly (6), wherein the injector sub-assembly is located within the housing; the injector sub-assembly includes a needle (20), a syringe barrel (18) and a piston (40) located within the syringe barrel; the injector sub-assembly is slidably mounted within the housing between an operative configuration in which at least a portion of the needle projects from the housing, and a retracted configuration in which the injector sub assembly is wholly located within the housing; and wherein the housing includes a housing body and needle exit door (44) pivotally connected to the body such that the door closes a needle exit aperture defined by the housing body when the injector sub-assembly is in its retracted configuration and opens when the injector sub-assembly is in its operative configuration to permit the needle to exit the housing.

Abstract: A line of sight antenna supported in an upturned terminal winglet or similar vertical member of an aircraft is disclosed. An aperture is formed in the conductive winglet or vertical member, and the antenna is supported within the aperture by a support mechanism such that the antenna is exposed to the line of sight transmissions. A non-conductive covering may also be used for the aperture. Using the cover, the antenna within the winglet can be configured so that it does not alter the appearance or aerodynamic characteristics of the aircraft. Alternatively, the antenna can be coupled to the outside of the winglet or vertical member if cosmetics are not a concern. The frequency range of the antenna can be tuned to cover desired frequency ranges. The antenna position at the winglet maintains a large physical separation from fuselage-mounted antennas thereby reducing interference.

Abstract: A line of sight antenna supported in an upturned terminal winglet or similar vertical member of an aircraft is disclosed. An aperture is formed in the conductive winglet or vertical member, and the antenna is supported within the aperture by a support mechanism such that the antenna is exposed to the line of sight transmissions. A non-conductive covering may also be used for the aperture. Using the cover, the antenna within the winglet can be configured so that it does not alter the appearance or aerodynamic characteristics of the aircraft. Alternatively, the antenna can be coupled to the outside of the winglet or vertical member if cosmetics are not a concern. The frequency range of the antenna can be tuned to cover desired frequency ranges. The antenna position at the winglet maintains a large physical separation from fuselage-mounted antennas thereby reducing interference.