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Initial mass in low Earth orbit (IMLEO) as a function of mission DV, engine type and tankage weight fraction r

Chemical engines

Tankage fraction = 1 A = 0.05""" Tankage fraction : A = 0.10

Initial mass in low Earth orbit (IMLEO) as a function of mission DV, engine type and tankage weight fraction r

Chemical engines

Tankage fraction = 1 A = 0.05""" Tankage fraction : A = 0.10

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