Enabling Sustainable Habitation at the Lunar Base

are the volume, power, cooling and crewtime mass equivalency factors, respectively per the mission segment of interest.(Used to convert the non-mass parameters (V, P, C and CT) to mass equivalencies.- D is mission segment duration.-- M, V, P, C and CT are the mass, volume, power, M, V, P, C and CT are the mass, volume, power, cooling and crewtime needs, respectively, of the system of interest.-- VV