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				| 1. | A rocket whose initial mass is 850 kg consumes fuel at the rate of 2.3 kgs-1, The speed of the exhaust gases relative to the rocket engine is 2000 ms-1. What thrust does the rocket engine provide? | 
| A. | 5.47 x 106 N | 
| B. | 4600 N | 
| C. | 1217 N | 
| D. | 6440 N | 
| Answer» C. 1217 N | |