发明名称 Launching long range aerial missile from submerged submarine
摘要 The composite, amphibious, tactical missile (2) is self-propelled on issuing from the submarine (1). It is hermetically enclosed in an envelope (10). The underwater trajectory (3) is continuously controlled, as is the initial part of the aerial trajectory, by means of jet spoilers (8) governed by an inertia-type data generator. - Emergence of the envelope from the water (4) is ensured at a predetermined velocity and angle to the horizontal. The missile is released from its envelope at a predetermined altitude above sea level (4). The wings (32) and control surfaces are extended and the missile is guided to the target. The rear section of the missile has amplifiers in a motor compartment to control the jet spoilers and a computer giving commands to the amplifiers.
申请公布号 ES2001374(A6) 申请公布日期 1988.05.16
申请号 ES19860001125 申请日期 1986.08.14
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 STAUFF EMILE;GUILLOT JEAN;PINEL ANDRE
分类号 F41F3/10;F42B15/20;(IPC1-7):F41F3/10 主分类号 F41F3/10
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