A designer is designing an aircraft which has climb gradient of 1.5 an – McqOptions

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1.	A designer is designing an aircraft which has climb gradient of 1.5 and has drag of 20N. If it weighs 220kg then, determine thrust to weight ratio?
A.	0.097
B.	0.87
C.	20
D.	220
Answer» B. 0.87

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