Estimation of the mass of the centrifugal electric pump unit of the spacecraft thermal control system
Alexandr Bobkov
Abstract:The article deals with the problem of estimating the mass of a centrifugal electric pump unit of a spacecraft thermal control system at the stage of preliminary design. The energy parameters of the electric pump are considered as the initial information relevant for the specified assessment: mass and volume flow V(m3/sec), head H (Joule/kg) and speed factor ns (dimensionless parameter). Based on the known data, using a third-order equation, an approximation of the graphical dependence of the reduced mass Mm of… Show more
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