GATE_AE_2027_MOCK_04_Q48 GATE 2027 Aerospace Engineering All-India Master Mock 04 (Aerospace Structures, Thin-Walled Beams & Aeroelasticity) NAT · 2 Marks
Flight Mechanics & Space Dynamics • Atmospheric Flight Mechanics • Glide and Climb Performance

An aircraft of weight W = 60 kN has available excess power P_{excess} = 600 kW at sea level. What is the maximum rate of climb (R/C) in m/s?

Answer Key:
10

Step-by-Step Verified Solution

### Solution: Rate of climb R/C = P_{excess} / W = 600000 W / 60000 N = 10 m/s. Correct: 10.
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