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				| 1. | Find the approximate value of climb angle if Thrust is 1500N, drag is 1000N and weight of the aircraft is 2500N. | 
| A. | 11.53 degree | 
| B. | 30 degree | 
| C. | 40 degree | 
| D. | 1 degree | 
| Answer» B. 30 degree | |