Javelin - Close Combat Missile System, Medium (FM 3-22.37) by George W. Casey

By George W. Casey

Руководство по ракетной системе ближнего боя Javelin (Джавелин) Армии США. (спецификации, обслуживание и применение). This e-book presents technical info, education innovations, and assistance at the present Javelin weapon procedure and Block 1 advancements. The meant clients contain unit leaders, running shoes, and unique gunners. The clients will locate this data helpful of their efforts to effectively combine this weapon procedure into their wrestle operations.

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Extra resources for Javelin - Close Combat Missile System, Medium (FM 3-22.37)

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This control changes the angle of thrust from the flight motor, resulting in a change to the missile’s flight path. 37 20 March 2008 Introduction Thermal Battery 1-50. The thermal battery provides internal electrical power for the missile during flight. It is sealed in the body of the missile. Figure 1-25. Control actuator section. CAPABILITIES AND FEATURES 1-51. The missile has two gunner-selectable attack modes: top or direct. Each mode has its own flight path or profile for reaching the target.

The control actuator section consists of four control fins, four thrust vector control (TVC) vanes, and a thermal battery. Control Fins 1-48. The control fins maneuver the missile during flight. The spring-loaded fins automatically deploy and lock into flight position after the missile clears the LTA. During flight, they adjust automatically to guide the missile to the target. Thrust Vector Control Vanes 1-49. The TVC vanes aid the control fins in maneuvering the missile during flight by deflecting the flight motor exhaust.

The spring-loaded fins automatically deploy and lock into flight position after the missile clears the LTA. During flight, they adjust automatically to guide the missile to the target. Thrust Vector Control Vanes 1-49. The TVC vanes aid the control fins in maneuvering the missile during flight by deflecting the flight motor exhaust. This control changes the angle of thrust from the flight motor, resulting in a change to the missile’s flight path. 37 20 March 2008 Introduction Thermal Battery 1-50.

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