| 摘要 |
The invention is sensor pod assembly for mounting sensor systems for an aircraft, the aircraft having a fuselage with a longitudinal axis. In detail the sensor pod includes an elongated pod having front and rear ends, the pod removable mountable to the underside of the fuselage of the aircraft aligned with the longitudinal axis. A mounting system is includes to mount at least one container capable of being pressurized in a plurality of locations within the pod along the longitudinal axis, the at least one container including means to mount the sensor systems there within.
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