The propellant in the proposed PSLV rocket of | vedclass

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(C) The $PSLV$ (Polar Satellite Launch Vehicle) is a multi-stage rocket. It utilizes a combination of solid and liquid propellants in its different st

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$C$. Both $(A)$ and $(B)$ in different stages of rocket propulsion

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(C) The $PSLV$ (Polar Satellite Launch Vehicle) is a multi-stage rocket. It utilizes a combination of solid and liquid propellants in its different stages. Specifically,it uses composite solid propellants in the booster stages and liquid propellants (like $N_2O_4$ with $UDMH$ or $MMH$) in the liquid stages to achieve the required thrust and control. Therefore,both $(A)$ and $(B)$ are used in different stages of the rocket.

The propellant in the proposed $PSLV$ rocket of the Indian space programme shall consist of

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