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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 | |