What kind of rocket motor does the AGM-65 Maverick utilize?

The AGM-65 Maverick employs a dual thrust rocket motor, which is an important feature for its operational effectiveness. The dual thrust design allows the motor to deliver two phases of thrust, providing enhanced performance during flight. The initial thrust phase delivers a rapid acceleration, allowing the missile to quickly reach its target, while the second phase maintains a sustained thrust for additional range and stability. This type of motor is particularly effective for guided missile systems like the Maverick, which need to balance speed and endurance for effective target engagement.

In contrast, the other options represent different types of rocket motor technologies that do not apply to the Maverick. Single stage rockets would not provide the nuanced thrust control needed for precision targeting. Solid fuel motors, while used in various applications, do not offer the same level of thrust variation as dual thrust motors. Liquid propellant systems are also distinct in terms of design and operational requirements, and they are not utilized in the Maverick missile.