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

  • A
    $A$. $A$ composite solid propellant
  • B
    $B$. Biliquid propellants such as $N_2O_4 +$ unsymmetrical dimethyl hydrazine $(UDMH)$ and $N_2O_4 +$ monomethyl hydrazine $(MMH)$
  • C
    $C$. Both $(A)$ and $(B)$ in different stages of rocket propulsion
  • D
    $D$. Kerosene and liquid oxygen

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