Summary of Resources for the International Space Station Environmental Control and Life Support System 972332
The assembly complete Environmental Control and Life Support (ECLS) system for the International Space Station (ISS) will consist of components and subsystems in both the U.S. and International partner elements which together will perform the functions of Temperature and Humidity Control (THC), Atmosphere Control and Supply (ACS), Atmosphere Revitalization (AR), Water Recovery and Management (WRM), Waste Management (WM), Fire Detection and Suppression (FDS), and Vacuum System (VS) for the station. Due to limited resources available on ISS, detailed attention is given to minimizing and tracking all resources associated with all systems, beginning with estimates during the hardware development phase through measured actuals when flight hardware is built and delivered. A comprehensive summary of resources consumed by the U.S. ECLS system hardware is presented, including launch weight, average continuous and peak power loads, on-orbit volume, resupply logistics, and crew time for maintenance.
Citation: Carrasquillo, R., Reuter, J., and Philistine, C., "Summary of Resources for the International Space Station Environmental Control and Life Support System," SAE Technical Paper 972332, 1997, https://doi.org/10.4271/972332. Download Citation
Robyn L. Carrasquillo, James L. Reuter, Cynthia L. Philistine
NASA Marshall Space Flight Center, NASA Johnson Space Center, Boeing Company
International Conference On Environmental Systems