Given:
- Total mass of the aircraft, $m = 20$ Mg $= 20 \times 10^3$ kg
- Thrust from the main engines, $2T = 5$ kN $= 5 \times 10^3$ N
- Thrust from the nose engine, $T' = 2$ kN $= 2 \times 10^3$ N
- Distances from the center of mass G:
- Horizontal distance
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