A technique for launching a missile that avoids some of the costs and disadvantages for doing so in the prior art. In particular, the illustrative embodiment of the present invention uses an electromagnetic catapult to throw the missile clear of the launch platform with sufficient velocity to attain aerodynamic flight before the missile's engine is ignited.
申请公布号
WO2005019761(A2)
申请公布日期
2005.03.03
申请号
WO2004US24914
申请日期
2004.07.30
申请人
LOCKHEED MARTIN CORPORATION;ROOT, GEORGE, RAYMOND, JR.