An energy auditor is part of power operations
Answer:
a) specific impulse = 203 s
(b) mass flow rate = 2511 kg/s
(c) throat diameter = 0.774 m
(d) exit diameter = 1.95 m
(e) thrust = 5.3*10^6 N/m^2
(f) thrust at sea level = 15.6*10^6 N
(g) thrust with hydrogen = 5*10^6 N
(h) thrust with stagnation = 5*10^6 N
Explanation:
See the attached file for explanation.
Answer:
I’m sorry I don’t understand this is there more steps?♀️
Explanation:
Answer:
to determine the rate of heat loss from that wall by convection = 12780 watts
Explanation: