Propulsion/Control Modular Booster.
Patent, Filed 8 Sep 80, patented 21 Dec 82,
DEPARTMENT OF THE NAVY WASHINGTON DC
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A modular, apogee-control package is disclosed which can be added to existing missiles, and which will limit the apogee of the missile trajectory by implementation of thrust vector control TVC. The package comprises, a boost guidance unit, a solid rocket propellant motor, and jet vane TVC.
- Solid Propellant Rocket Engines
- Guided Missile Trajectories, Accuracy and Ballistics
- Guided Missiles