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27
AGRAS T30
Unmanned Aircraft Flight Manual
Center of Gravity Limitations
1. Using the M1 motor shaft as a reference, the aircraft center of gravity in the front-to-back direction
should be between 855-935 mm from the reference.
2. Using the lowest point of the aircraft as a reference, the aircraft center of gravity in the vertical
direction should be between 527-567 mm from the reference.
3. The aircraft center of gravity in the left-to-right direction should be the symmetrical center of the
aircraft.
Front Center of Gravity 855 mm
Rear Center of Gravity 935 mm
Wheelbase L1 1720 mm
Wheelbase L2 1885 mm
M1 M4
M2 M3
M6 M5
Aircraft Front
527 mm
567 mm
Center of Gravity
Without Load
Aircraft Front
Front Center of Gravity 855 mm
Rear Center of Gravity 935 mm
Wheelbase L1 1720 mm
Wheelbase L2 1885 mm
M1 M4
M2 M3
M6 M5
Aircraft Front
527 mm
567 mm
Without Load