VERFAHREN ZUM LENKEN EINES MIT NIEDRIGER GESCHWINDIGKEIT AUS EINEM ROHR ABGESCHOSSENEN FLUGKOERPERS UND WAFFENSYSTEM SOWIE FLUGKOERPER ZUR DURCHFUEHRUNG DIESES VERFAHRENS

A procedure for steering a missile launched at low speed from a tube, with the missile being equipped with a propulsion unit system of the type with a propellant fuel charge. The procedure is characterized by the fact that the above-mentioned propulsion unit system is determined and arranged in such...

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Bibliographic Details
Main Authors GUILLOT, JEAN, CHATENAY MALABRY, FR, RAYNAUD, JACQUES, SAVIGNY SUR ORGE, FR, VAILLANT, ROBERT, PARIS, FR, MAREE, MICHEL, GIF SUR YVETTE, FR, ANSALDI, JEAN, ST. REMY-LESVREUSES, FR
Format Patent
LanguageGerman
Published 08.01.1987
Edition4
Subjects
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A procedure for steering a missile launched at low speed from a tube, with the missile being equipped with a propulsion unit system of the type with a propellant fuel charge. The procedure is characterized by the fact that the above-mentioned propulsion unit system is determined and arranged in such a way that it can simultaneously impart to the missile axial propulsive thrust and maneuver forces for steering by force and that the variation of the position of the center of gravity of the missile on its axis as a function of the burn-up of the propellant charge is such that, when the missile leaves the tube, the center of gravity passes through the line of action of the above-mentioned maneuver forces and that, during its flight, makes it possible for torques to develop which generate aerodynamic angles of attack and which produce maneuver forces which are added to those of steering by force.
Bibliography:Application Number: DE19823221039