While designing the refrigeration system of an aircraft, the prime consideration is that the
a) System has high C.O.P.
b) Power per TR is low
c) Mass of refrigerant circulated in the system is low
d) Mass of the refrigeration equipment is low
While designing the refrigeration system of an aircraft, the prime consideration is that the
a) System has high C.O.P.
b) Power per TR is low
c) Mass of refrigerant circulated in the system is low
d) Mass of the refrigeration equipment is low
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