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If a rocket runs on a fuel (C 15 H 30 ) and liquid oxygen, the weight of oxygen required and CO 2 released for every litre of fuel respectively are : (Given : density of the fuel is 0.756 g/mL)
- 1188 g and 1296 g
- 2376 g and 2592 g
- 2592 g and 2376 g
- 3429 g and 3142 g
Correct answer: 2592 g and 2376 g
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