The initial mass of a rocket is \( 1000 \, \text{kg} \). Calculate at what rate the fuel should be burnt so that the rocket is given an acceleration of \( 20 \, \text{m s}^{-2} \). The gases come out at a relative speed of \( 500 \, \text{m s}^{-1} \) with respect to the rocket:
[Use \( g = 10 \, \text{m /s}^{2} \)]