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Lightweight and Regenerable CO₂ and H₂O Sequestration System

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NASA-SBIR-185616SBIR / STTR

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This contract focuses on the development of a lightweight and regenerable non-venting CO2 and H2O sequestration system designed for Portable Life Support Systems in partial-gravity environments. The architecture utilizes a spray-based absorption process with a low-viscosity ionic liquid and a gravity-independent Capillary Condensing Heat Exchanger to manage water vapor. By employing a low-power chemical stripping process that converts CO2 into a solid, the system maintains a closed loop that eliminates the need for energy-intensive vacuum desorption or gas compression. The design adheres to strict constraints, weighing approximately 9.2 lbm with a power consumption of 20 to 25 W, making it ideal for eight-hour extravehicular activities on Mars or the Moon. Managed by the NASA SBIR/STTR Program, this innovation supports long-duration missions by preserving critical water and oxygen resources and reducing reliance on Earth resupply. Beyond EVA suits, the technology has broad applications for space stations, habitats, and rovers, as well as terrestrial uses in submarines, mining, and industrial direct air capture. The project is structured as a total small business set-aside, aiming to advance environmental control and life support systems through high-efficiency, low-footprint resource management.

General Info

NASA SBIR contract for lightweight, regenerable CO2 and H2O sequestration for space missions.

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Organization & Contact Information

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AgencyNational Aeronautics and Space Administration → NASA SBIR/STTR Program
Contacts4 people available
OfficeUSA
Office AddressUSA
Contacts
Ryan E OgilvieProject Manager
Ryan JensonPrincipal Investigator
Jason L KesslerProgram Director
Carlos TorrezProgram Manager

Full Description

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The research introduces a compact, lightweight, and regenerable non-venting CO₂ and H₂O architecture for use in Portable Life Support Systems (PLSSs). The architecture integrates spray-based absorption and chemical stripping, featuring a novel gravity-independent Capillary Condensing Heat Exchanger (CCHX) to condense and separate water vapor. A fine-droplet spray reactor enhances CO₂ absorption into a low-viscosity ionic liquid (IL), maximizing efficiency while minimizing mass and volume. The CO₂-rich, droplet-laden flow then passes through a Multiplexed Inertial Filter (MIF), which captures and collects the IL for subsequent stripping and recirculation. For regeneration, a low-power chemical stripping process converts the CO₂ into a solid, storing it without venting. This approach eliminates the need for energy-intensive thermal/vacuum desorption or gas compression, maintaining a closed loop with continuous CO2 uptake and storage. The resulting solid can be reprocessed at a habitat, enabling repeated use. The system meets CO₂ and H₂O requirements for an eight-hour extravehicular activity while adhering to strict mass (<12 lbm) and volume (<10″×8″×5″) constraints critical for partial-gravity. By combining advanced transport technologies, lightweight materials, capillary-driven condensation, optimized IL spraying, and efficient chemical stripping, this design delivers superior resource efficiency, reduced mass, and reliable closed-loop CO₂/H₂O management. The approach diverges from traditional systems, which rely on solids or sorbents with water and high-energy regeneration requirements by leveraging water-free ILs and low-energy chemical sequestration. The significance of this innovation is profound for long-duration Mars missions: (1) By sequestering CO₂ and H₂O without venting, the system preserves water and oxygen—critical for EVA duration and habitat sustainability—reducing reliance on Earth resupply and enhancing mission autonomy. (2) With an onboard mass of ~ 9.2 lbm during EVA the system beats the < 12 lbm limit, and net power consumption of ~ 20–25 W, it aligns with PLSS constraints, enabling lightweight, energy-efficient designs for extended EVAs. (3) The water-free, thermally stable Ionic Liquid and non-volatile nature are ideal for Mars. (4) The closed-loop recycling at the habitat regenerates chemicals supporting long-term operations and reducing waste. (5) The system advances PLSS capabilities beyond current state-of-the-art offering a non-venting, regenerable solution.
Benefits: A compact, lightweight, non-venting CO₂/H₂O system offers NASA multiple applications. For EVA suits, its low mass and small size suit lunar/Mars missions, preserving resources without venting. In habitats, its closed-loop design and solid CO₂ storage support ISRU, recovering water and enabling O₂ production with low power. For deep space missions, it ensures air quality and water recovery in microgravity, cutting launch mass and consumables. On space stations, it enhances CO₂ scrubbing and sustainability. It could serve as an emergency backup in spacecraft/habitats, sustaining crews during ECLSS failures. For commercial spaceflight, it fits cost-efficient suits/habitats. Aligning with Artemis and Mars goals, this system boosts resource efficiency and sustainability in space. This system integrates multiple advanced technologies for a wide range of applications. At its core is a compact, power-efficient spray-based CO₂ capture process, suitable for both Earth-based and extraterrestrial Environmental Control and Life Support Systems (ECLSS). In space, it can be used for portable life support systems, space stations, habitats, rovers, and spacecraft where CO₂ scrubbing is essential—offering clear advantages for commercial space ventures. On Earth, potential uses include air revitalization in enclosed or harsh environments such as SCUBA operations, mining, and submarines. The system’s compact design further enables specialized implementations, for aviation, while larger-scale applications, such as Direct Air Capture and industrial CO₂ containment processes, can also benefit from its high-efficiency, low-footprint approach.

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