1.

What is the nozzle throat diameter of a rocket having chamber pressure (Pc) of 3 MPa, mass flow rate (m) of 20 kg/s and characteristic velocity (c*) of 1500 m/s?

A. 10 cm
B. 11.3 cm
C. 12.8 cm
D. 25 cm
Answer» C. 12.8 cm


Discussion

No Comment Found