Mass Economy Evaluation for Integrated ECLSS and Propulsion ArchitectureAs missions in low Earth orbit (LEO) lengthen and extend to deep space, minimizing resupply needs becomes vital for sustaining crewed operations. Traditional life support systems depend on consumables resupplied from Earth, a method that is increasingly impractical for missions beyond LEO, such as lunar outposts or Mars transit. Long-duration missions require more efficient, autonomous systems that can recycle essential resources, particularly water and oxygen, to minimize the frequency and mass of resupply missions.
The Environmental Control and Life Support System (ECLSS) is essential to such missions, with the International Space Station (ISS) serving as a testbed for advanced water recovery and partial oxygen recycling via physico-chemical methods. Yet, ECLSS and propulsion subsystems generally operate independently, despite overlapping requirements and potential areas for synergy. For instance, ECLSS byproducts, water, CO2, and hydrogen, could be repurposed for propulsion, potentially reducing dedicated propellant mass and increasing overall system efficiency.
One promising approach is to develop shared-resource architectures that integrate ECLSS with propulsion systems. This study examines the potential of such integration through the Sabatier CO₂ reduction process, focusing on water management as a key factor in system mass trade-offs. The Sabatier reaction produces water and methane from metabolic CO2 and electrolytic hydrogen, partially closing the life support loop and providing methane, which could serve as a propellant. This integration could minimize waste, reduce resupply requirements, and enhance mission mass efficiency.
A dynamic modeling framework will be used to simulate resource flows over long missions, capturing interactions between life support and propulsion. By comparing integrated versus separate system configurations, the study aims to quantify mass benefits and penalties, informing future habitat designs and trade studies for missions prioritizing autonomy and mass efficiency.
Document ID
20260005378
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Leon Chen (The Aerospace Corporation El Segundo, United States)
Alicia Rangel (Johnson Space Center Houston, United States)
Date Acquired
June 15, 2026
Publication Date
July 12, 2026
Publication Information
Publisher: International Conference on Environmental Systems
Subject Category
Man/System Technology and Life Support
Report/Patent Number
ICES-2026-190
Meeting Information
Meeting: 55th International Conference on Environmental Systems (ICES)
Location: Rio Grande
Country: PR
Start Date: July 12, 2026
End Date: July 16, 2026
Sponsors: International Conference on Environmental Systems