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AIAA SPACE 2013 Conference and Exposition
Nomenclature α = function of Technology Readiness Level (TRL) β = complexity of each connection between pairs of components γ = 1/n Π i = expected profit for missions of type i A = Design Structural Matrix C AIT = assembly, integration, and test cost C D = development cost of each satlet variant C NR = non-recurring development costs C PMSE = aggregate system level PMSE estimate C i R = recurring costs (manufacturing costs, operations costs, and launch costs) C 1 = complexity due to number anddoi:10.2514/6.2013-5371 fatcat:nsad3g263zb47df737zuov4w24