The relationship between the specific impulse of a rocket $(I_s)$ and the critical temperature $(T_c)$ of the fuel reacted in the rocket motor is:

  • A
    $I_s \propto T_c$
  • B
    $I_s \propto 1/T_c$
  • C
    $I_s \propto \sqrt{T_c}$
  • D
    $I_s \propto \sqrt{1/T_c}$

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Similar Questions

Match List-$I$ with List-$II$ and select the correct answer using the codes given below the lists.
List-$I$ (Compounds) List-$II$ (Used in)
$A$. $BaSO_4 + ZnS$ $1$. Explosive
$B$. $NI_3$ $2$. Oxidiser in rocket propellants
$C$. $N_2O_4$ $3$. Space capsule
$D$. $KO_2$ $4$. Pigment

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.

Which of the following could act as a propellant for a rocket?

Which of the following is used as an oxidiser in rocket propellants?

Which of the following is used as an oxidant with liquid propellant?

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