A crankshaft damper and a method of crankshaft damper assembly using interlocking beads. In this case, the invention provides for a flow deflection device, which is not the same as the blowing device and which deflects the quenching gas flow radially outward through more than 90, to be provided in the outlet-flow area of the quenching gas. The disclosed technology provides a method for copying the unduplicated information without transmitting or storing the duplicated portions. A controller controls the transfer of propellant from within the exchangeable propellant cartridge system to the spacecraft. The second semiconductor die defines a second active surface, the second active surface includes at least one conductive bond pad.