1.

What are the standardized chamber pressure and exit pressure values used for comparing the specific impulse values or various design parameters of different rocket engines?

A. 1000 psia, 1 atm
B. 1000 atm, 1 psia
C. 100 psia, 1 atm
D. 100 atm, 1 psia
Answer» B. 1000 atm, 1 psia


Discussion

No Comment Found