Viking 4 is Snecma Moteurs’ storable-propellant liquid rocket engine for the Ariane second stage. ESA’s Ariane 4 reference identifies a single Viking 4 using nitrogen tetroxide and UH25, with 798 kN engine thrust and a 125-second stage firing. That upper-stage figure describes the named Ariane 4 installation; it should be read separately from the first-stage Viking 5 and liquid-booster Viking 6 ratings. The Ariane 4 vehicle family completed service in 2003.