Which is the relation between the specific im | vedclass

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(C) In the context of rocket propulsion and propellant chemistry,the specific impulse ${I_s}$ is a measure of the efficiency of the propellant. For a

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${I_s} \ge T_c^{1/2}$

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(C) In the context of rocket propulsion and propellant chemistry,the specific impulse ${I_s}$ is a measure of the efficiency of the propellant. For a stable and effective rocket blast,the specific impulse must satisfy the condition ${I_s} \ge T_c^{1/2}$,where ${T_c}$ is the critical temperature of the combustion process. Therefore,option $C$ is the correct relationship.

Which is the relation between the specific impulse ${I_s}$ and the critical temperature ${T_c}$ attained in a rocket blast?

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