Aerospace Engineering > GATE 2009 > Climb Performance
An aircraft of mass 2500 kg in straight and level flight at a constant speed of 100 m/s has available
excess power of 1.0×106 W. The steady rate of climb it can attain at that speed is
excess power of 1.0×106 W. The steady rate of climb it can attain at that speed is
Correct : c
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