Propulsion/Control Modular Booster

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Propulsion/Control Modular Booster

Propulsion/Control Modular Booster

M. J. Ripley-Lotee / R. B. Dillinger / K. E. Clark

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. (Author)

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Title :

Propulsion/Control Modular Booster

Contributors:

M. J. Ripley-Lotee (author) / R. B. Dillinger (author) / K. E. Clark (author)

Publication date :

1980

Size :

17 pages

Type of media :

Report

Type of material :

No indication

Language :

English

Keywords :

Rocket Engines & Motors , Missile Technology , Ordnance , Patent applications , Solid propellant rocket engines , Thrust vector control systems , Guidance , Inventions , Guided missiles , Guided missile trajectories , Boost phase , Trajectories , Jet vanes

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