$A$ space rocket is propelled by

  • A
    An automobilic engine
  • B
    Nuclear engine
  • C
    Steam engine
  • D
    Mixture of fuel and oxidiser called propellant

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Similar Questions

What is the reason for adding glycerol to aviation fuel?

Which of the following is not used in rocket propellants?

Solid fuel used in rockets is a mixture of $Fe_2O_3$ and $Al$ (in ratio $1:2$ by moles). The heat evolved $(kJ)$ per gram of the mixture is $............$. (Nearest integer)
Given: $\Delta H_{f}^{\ominus}(Al_2O_3) = -1700 \ kJ \ mol^{-1}$
$\Delta H_{f}^{\ominus}(Fe_2O_3) = -840 \ kJ \ mol^{-1}$
Molar mass of $Fe$,$Al$ and $O$ are $56$,$27$ and $16 \ g \ mol^{-1}$ respectively.

What is the reason for adding glycerol to aviation fuel?

Which of the following acts as a rocket propellant?

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