8D715P is the Kosberg RD0108 LOX/kerosene liquid rocket engine developed by OKB-154 (JSC KBKhA) for the 11A57 Voskhod Block I third stage. KBKhA lists 30.38 tf vacuum thrust (normalized here to 297.9 kN), 326 s specific impulse, and production at Factory No. 154 (VMZ); NASA dates its first use to 1963. This historical model remains distinct from the RD-0109/8D719 engine used on the earlier Block Ye stage.