1.

A 5000 kg rocket is set for vertical firing. The exhaust speed is \[800\,m{{s}^{-1}}\]. To give an initial upward acceleration of \[20\,m{{s}^{-2}}\], the amount of gas ejected per second to supply the needed thrust will be \[(g=10\,m{{s}^{-2}})\] [CBSE PMT 1998]

A. \[127.5\,kg\,{{s}^{-1}}\]
B. \[187.5\,kg\,{{s}^{-1}}\]
C. \[185.5\,kg\,{{s}^{-1}}\]
D. \[137.5\,kg\,{{s}^{-1}}\]
Answer» C. \[185.5\,kg\,{{s}^{-1}}\]


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