An aircraft, comprising: a fuselage; a propulsion system operatively coupled to the fuselage; and an aerial refueling system coupled to the fuselage and including: a tank adapted to contain a flowable material; a conduit operatively coupled to the tank and being adapted to receive the flowable material and to facilitate transfer of the flowable material between the tank and a second location, the conduit including a wall member; and characterized in that it further comprises a plurality of reflective members being at least one of formed within an outer layer of the wall member and disposed on an outer surface of the wall member, the reflective members being adapted to at least partially reflect light incident thereon, wherein the wall member includes a first portion and a second portion, the first portion having a first concentration of reflective members and the second portion having a second concentration of reflective members and wherein the first concentration of reflective members is greater than the second concentration of reflective members, wherein the second portion includes a marking on the wall member corresponding to an outer refueling limit of the aerial refueling system, and wherein the second portion includes a marking on the wall member corresponding to an inner refueling limit of the aerial refueling system. a fuselage; a propulsion system operatively coupled to the fuselage; and an aerial refueling system coupled to the fuselage and including: a tank adapted to contain a flowable material; a conduit operatively coupled to the tank and being adapted to receive the flowable material and to facilitate transfer of the flowable material between the tank and a second location, the conduit including a wall member; and characterized in that it further comprises a plurality of reflective members being at least one of formed within an outer layer of the wall member and disposed on an outer surface of the wall member, the reflective members being adapted to at least partially reflect light incident thereon, wherein the wall member includes a first portion and a second portion, the first portion having a first concentration of reflective members and the second portion having a second concentration of reflective members and wherein the first concentration of reflective members is greater than the second concentration of reflective members, wherein the second portion includes a marking on the wall member corresponding to an outer refueling limit of the aerial refueling system, and wherein the second portion includes a marking on the wall member corresponding to an inner refueling limit of the aerial refueling system. a tank adapted to contain a flowable material; a conduit operatively coupled to the tank and being adapted to receive the flowable material and to facilitate transfer of the flowable material between the tank and a second location, the conduit including a wall member; and characterized in that it further comprises a plurality of reflective members being at least one of formed within an outer layer of the wall member and disposed on an outer surface of the wall member, the reflective members being adapted to at least partially reflect light incident thereon, wherein the wall member includes a first portion and a second portion, the first portion having a first concentration of reflective members and the second portion having a second concentration of reflective members and wherein the first concentration of reflective members is greater than the second concentration of reflective members, wherein the second portion includes a marking on the wall member corresponding to an outer refueling limit of the aerial refueling system, and wherein the second portion includes a marking on the wall member corresponding to an inner refueling limit of the aerial refueling system.