Turbojet Engine Bus Vehicle Section
Item Name Code (INC) 68689
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An item consisting of one turbo jet Engine, housed inside an aerodynamic shell or skin, designed to provide the thrust required to power the target through it's subsonic phase of flight. It includes either moveable control surface(s), stabilizing fins, or wings. It is designed to mate with other sprint vehicle sections.
Additional Information for Turbojet Engine Bus Vehicle Section
The Turbojet Engine Bus Vehicle Section is a component of the Guided Missile system. It is classified under the supply class Guided Missile Components, which falls under the supply group Guided Missiles.
The Turbojet Engine Bus Vehicle Section is responsible for providing the necessary propulsion and power to the guided missile. It consists of a turbojet engine, which generates thrust by compressing and combusting air with fuel. The bus vehicle section also includes various subsystems and components, such as fuel tanks, fuel pumps, control systems, and electrical systems, which are essential for the operation and control of the guided missile.
Overall, the Turbojet Engine Bus Vehicle Section plays a crucial role in the functioning of the guided missile, providing the necessary power and propulsion for its flight and maneuverability.
Related Item Names for INC 68689 Turbojet Engine Bus Vehicle Section
NATO Stock Numbers with Item Name 68689 Turbojet Engine Bus Vehicle Section Page 1 of 1
- 016191730
- TD110824
- RNCC: 3 | RNVC: 2
