发明名称 Method for safe flight testing of high velocity interceptor missiles
摘要 An intercept missile testing method which includes the steps of launching a test missile threat from a first location on a substantially vertical trajectory, e.g., with a flight path angle greater than about 70 DEG , towards an intercept point, and launching a test intercept missile from a second location on a substantially vertical trajectory, e.g., with a flight path angle greater than about 70 DEG , towards the intercept point. The flight paths are selected so that the test intercept missile will intercept the test missile threat exoatmospherically, at an intercept (engagement crossing) angle of less than about 30 DEG . Preferably, the launch velocities and trajectories of the test intercept missile and the test missile threat are selected so that the intercept will occur exoatmospherically when the test missile threat is on a downward trajectory at a velocity of 5-8 km/sec, while the test intercept missile is on an upward trajectory at a velocity 5-9 km/sec. The first location is preferably Wake Island, Johnston Island, or Kauai, and the second location is preferably Meck Island.
申请公布号 US5866837(A) 申请公布日期 1999.02.02
申请号 US19970878124 申请日期 1997.06.18
申请人 MCDONNELL DOUGLAS CORPORATION 发明人 BIVEN, EARL U.;MIKELSON, GARY C.;SCAPELLATI, GARY A.
分类号 F41G7/00;(IPC1-7):B64D1/04 主分类号 F41G7/00
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