发明名称 Low mass flow reaction jet
摘要 A control system for a flying vehicle in an atmospheric environment, the vehicle having an aerodynamic shape including a front end and a rear end including a plurality of attitude control jet nozzles spaced outward from the vehicle near the rear end of the vehicle or a trailing edge of a vehicle part; and a generator for providing a low mass flow of a fluid through the attitude control jet nozzles to create an area of high pressure immediately forward of the nozzles and adjacent the flying vehicle, wherein the location of the attitude control jet nozzles is so close to the rear end of the vehicle that any area of low pressure created by the low mass flow of fluid through the attitude control jet nozzles does not contact the vehicle.
申请公布号 US6752351(B2) 申请公布日期 2004.06.22
申请号 US20020287020 申请日期 2002.11.04
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 JOHN LAWRENCE E.
分类号 F02K9/82;(IPC1-7):F41G7/00;F42B15/00 主分类号 F02K9/82
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