Arthur/Zoekeend-Phrase-Indexing
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Zoekeend-Phrase-Indexing/half_split2/208.tsv
Arthur Idema 4b675a151d Added sign test, updated results,
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1208what is the effect of the shape of the drag polar of a lifting spacecraft on the amount of reduction in maximum deceleration obtainable by continuously varying the aerodynamic coefficients during re-entry .