What initial mass of 210 po is needed in a space rtg with

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Reference no: EM13619350

What initial mass of 210 Po is needed in a space RTG with a 19% thermal to electric conversion efficiency that is to have a power output of 65 W(e) one year after the start of the mission?

Reference no: EM13619350

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What initial mass of 210 po is needed in a space rtg with : what initial mass of 210 po is needed in a space rtg with a 19 thermal to electric conversion efficiency that is to
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