FRAKOPLINGSBAR SKYVEKRAFT-VEKTORMEKANISME FOR ET MISSIL

A detachable thrust vector mechanism for a missile is disclosed comprising a plurality of motors mounted on a C-ring near the missile's aft end and synchronously moved with the missile's fins. The mechanism provides initial thrust and thrust vector control during an initial launch period....

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Bibliographic Details
Main Authors PHILLIPS, BILLY R, PEOPLES, JOHN R
Format Patent
LanguageNorwegian
Published 17.01.1990
Edition4
Subjects
AIRCRAFT
AMMUNITION
AVIATION
BLASTING
COSMONAUTICS
EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
HEATING
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
WEAPONS
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Summary:A detachable thrust vector mechanism for a missile is disclosed comprising a plurality of motors mounted on a C-ring near the missile's aft end and synchronously moved with the missile's fins. The mechanism provides initial thrust and thrust vector control during an initial launch period. The C-ring is adapted to transfer the thrust provided by the motors through the missile's aft end. The mechanism will remain automatically connected to and disengage from the missile without elaborate electro-mechanical action.
Bibliography:Application Number: NO19860003455