TMM management for mission support and TCS on-orbit verification

Abstract

In 2010 the Columbus module completed two years orbital operations on early 2010. Thermal and hydraulic aspects provided a challenging test bench for the engineering team supporting the flight operation, in terms of time response, correct prediction and interpretation of to the various issues raised. Evaluations for future payloads, stages and support to daily activities are the main areas involving the engineering support. Most of these tasks rely on the use of dedicated mathematical models, originally developed to support the review phases, from development to acceptance and fitted to current flight configuration. NomenclatureAPCU = Autonomous Power Control Unit APM = Attached Pressurized Module ATCS = Active Thermal Control System CDR = Critical Design Review CFA = Cabin Fan Assembly CHX = Condensing Heat Exchanger CR = Change Request CTS = Cabin Temperature Sensor DB = Dead Band DMS = Data Management System DPSB = Delta Pressure Sensor block EATCS = External Active Thermal Control System ECLSS = Environmental Control Life Support System ECS = Environmental Control System ECTMM = External Complement Thermal Mathematical Model EDR = European Drawer Rack EPC = Electronic Package Controller EPM = European Physiology Module ER-3 = Express Rack 3 ESA = European Space Agency EWACS = Emergency Warning & Caution System FAR = Flight Acceptance Review FCT = Flight Control Team FDIR = Failure Detection Isolation and Recovery FPR = Flight Prototype Rack FSL = Fluid Science Laboratory GMT = Greenwich Mean Time HRF = Human Research Facility ICD = Interface Control Document IOT = Industrial Operator Team IOTMM = Integrated Overall Thermal Mathematical Model ISPR = International Standard Payload Rack ISS = International Space Station LT = Low Temperature LTA = Launch to Activation MSG = Microgravity Sciences Glovebox MT = Medium Temperature PCTMM = Pressurized Complement Thermal Mathematical Model PDGF = Power Distribution Grapple Fixture PDR = Preliminary Design Review PFM = Proto Flight Model PICA = Pre-Integrated Columbus APM PID = Proportional Integrative Derivative PTCS = Passive Thermal Control System QR = Qualification Review REF = Radiative Exchange Factors SPR = System Problem Report SSRMF = Space Station Remote Manipulator System TAS-I = ThalesAlenia Space Italia TCS = Thermal Control System TCV = Temperature Control Valve THMM = Thermal-Hydraulic Mathematical Model TMM = Thermal Mathematical Model WFSV = Water Flow Selection Valve WLTS = Water Loop Test Step WMV = Water Modulating Valve WOOV = Water On Off Valve WPA = Water Pump Assembly WPU = Water Pump Unit WTSB = Wet Temperature Sensor Block Downloaded by CARLETON UNIVERSITY LIBRARY on July 30, 2015 | http://arc.aiaa.org |