发明申请
US20050011989A1 MISSILE CONTROL SYSTEM AND METHOD 有权
MISSILE控制系统和方法

MISSILE CONTROL SYSTEM AND METHOD
摘要:
A jet propulsion outlet device is disclosed that has a grid plate having a plurality of densely clustered nozzlettes, the nozzlettes of the grid plate being configured to operably couple to a pressurized gas source to efficiently expand the pressurized gas.
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