What is the primary purpose of the AGM-65's dual thrust rocket motor?

The primary purpose of the AGM-65's dual thrust rocket motor is to allow for variable propulsion. This design feature enables the missile to operate at two different thrust levels during its flight. The initial thrust provides the necessary acceleration to launch the missile quickly and reach a target altitude, while the reduced thrust maintains flight efficiency over longer distances.

This variable propulsion system is crucial for optimizing performance in various phases of the missile’s trajectory. It not only helps in achieving quicker launches but also supports flight range and overall maneuverability without the need for separate systems to address these different flight phases. The flexibility in thrust allows the AGM-65 to adapt to differing mission profiles effectively, making it a versatile weapon in operational scenarios.