The 3M54-1 uses a two-stage propulsion system for versatile performance. At launch, a solid rocket booster propels the missile from its platform, ensuring stable and rapid ascent. In the cruise phase, the missile transitions to a turbojet engine powered by liquid hydrocarbon fuel, enabling sustained flight at subsonic speeds of 0.8–0.9 Mach. The missile’s range is approximately 220–300 kilometers, varying based on its flight profile and payload configuration. During the terminal phase, a secondary propulsion system activates, accelerating the missile to supersonic speeds of up to 2.9 Mach. This final sprint not only enhances the missile’s impact force but also reduces the reaction time available to enemy air defenses, improving the likelihood of a successful strike.