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Which mechanism maintains constant spacecraft internal temperature, using radiative equivalence?

A)Selective emissivity radiative heat transfer
B)Forced convection air dilution refrigeration
C)Thermoelectric Peltier effect adjustment
D)Passive conduction heat spreader deployment

💡 Explanation

Selective surface emissivity uses radiative heat transfer because emitted radiation balances absorbed solar radiation, maintaining equivalent thermal energy; therefore, the net temperature remains stable, rather than relying on convection cooling or conduction alone.

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