1.

Specific impulse of a rocket and the critical temperature of the fuel reacted in the motor of the rocket has the relationship

A.                 \[{{I}_{s}}\propto {{T}_{c}}\]      
B.                 \[{{I}_{s}}\propto 1/{{T}_{c}}\]
C.                 \[{{I}_{s}}\propto \sqrt{\left( {{T}_{c}} \right)}\]               
D.                 \[{{I}_{s}}\propto \sqrt{(1/{{T}_{c}})}\]
Answer» D.                 \[{{I}_{s}}\propto \sqrt{(1/{{T}_{c}})}\]


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