Aerospace Engineering > GATE 2011 > Climb Performance
An aircraft with a mass of 5000 kg takes off from sea level with a forward speed of 50 m/s and
starts to climb with a climb angle of 15o. The rate of climb and excess thrust available at the start of
the climb respectively (assume g=9.81 ms-2) are
starts to climb with a climb angle of 15o. The rate of climb and excess thrust available at the start of
the climb respectively (assume g=9.81 ms-2) are
Correct : b
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