发明名称 CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY
摘要 A clustered, fixed cant, throttleable rocket assembly (102) is used to propel and a steer a vessel (100) in terrestrial or extraterrestrial applications. The fixed cant of each of at least three individual rocket engines (104, 106, 108) in the cluster provides the steering input to the overall assembly (102). More specifically, by changing the propellant flow rate to the individual rocket engines (104, 106, 108) relative to one another, the overall thrust vector of the rocket assembly (102) may be selected to provide a desired steering input to the vessel (100). A measured vessel orientation may be compared with a desired vessel orientation to determine what steering input is required to achieve the desired vessel orientation.
申请公布号 WO2013105988(A3) 申请公布日期 2013.09.26
申请号 WO2012US25308 申请日期 2012.02.15
申请人 FIRESTAR ENGINEERING, LLC;FISHER, DAVID;MUNGAS, GREGORY 发明人 FISHER, DAVID;MUNGAS, GREGORY
分类号 F02K9/00;F02K9/26;F02K9/30;F02K9/42 主分类号 F02K9/00
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