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 lowC-mass of refrigerant circulated in the system is lowD-mass of the refrigeration equipment is low-D-mass of the refrigeration equipment is low

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D mass of the refrigeration equipment is low Explanation: No answer description is available.

Heat Transfer Refrigeration and Air Conditioning

While designing the refrigeration system of an aircraft, the prime consideration is that the

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Heat Transfer Refrigeration and Air Conditioning

While designing the refrigeration system of an aircraft, the prime consideration is that the

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For help Students Orientation Mcqs Questions

For help Students Orientation
Mcqs Questions