From Handwiki Characteristic velocity or [math]\displaystyle{ c^* }[/math], or C-star is a measure of the combustion performance of a rocket engine independent of nozzle performance, and is used to compare different propellants and propulsion systems. c* should not be confused with c, which is the effective exhaust velocity related to the specific impulse by: [math]\displaystyle{ I_s = \frac{c}{g_0} }[/math]. Specific Impulse and effective exhaust velocity are dependent on the nozzle design unlike the characteristic velocity, explaining why C-star is an important value when comparing different propulsion system efficiencies. c* can be useful when comparing actual combustion performance to theoretical performance in order to determine how completely chemical energy release occurred. This is known as c*-efficiency.
[math]\displaystyle{ c^* = \frac{p_1A_t }{\dot{m}} }[/math]
[math]\displaystyle{ c^* = \frac{I_sg_0}{C_F} = \frac{c}{C_F} =\sqrt{\frac{RT_1}{k} \Bigl(\frac{k+1}{2}\Bigr)^{\frac{k+1}{k-1}}} }[/math]
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Categories: [Rocketry] [Rocket propulsion] [Aerospace engineering]
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