NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Thermal Radiator for CO2 Deposition in Deep Space Transit (FY21 XHab Final Report - University of North Texas)This UNT Senior design team was tasked by NASA to develop a variable conductance thermal radiator prototype for CO2 deposition for deep space transit. NASA selects university teams every year to partake in the X-HAB Academic Innovation Challenge, with this year’s number of teams being six. Air Revitalization is a crucial system for any space travel, be it for Low Earth Orbit, such as the International Space Station, or for deep space transit. Current systems, such as the Carbon Dioxide Removal Apparatus aboard the ISS, require upkeep and maintenance, which cannot be done on long distance space missions. For the past several years, NASA has done research on Cryogenic systems for Carbon Dioxide removal. These systems operate on the fact that Carbon Dioxide freezes at a higher temperature than Oxygen and Nitrogen, so Carbon Dioxide can be frozen out of the cabin atmosphere without the use of filters, which degrade over time. To cool the cabin air down to a temperature where Carbon Dioxide freezes, Stirling cryocoolers have been used, which have shown promise in the hope of Carbon Dioxide deposition for Cabin Air Revitalization. Cryogenic systems are much more reliable but require significant energy input to operate. Physical systems, such as radiators, have generally not been used for this task, as there is a need to be able to “turn off” the rejection of heat to allow the frozen carbon dioxide to be collected. However, with working fluids pumped through a physical radiator, that aspect of operation can be achieved. The goal of this challenge is to determine the effectiveness of a variable conductance thermal radiator that can reject heat to deep space, without the use of a dedicated cryocooler to remove energy from the cabin air. The proposed design uses piping, hot and cold working fluids, and non-condensable gas to absorbl heat from the cabin air on one side of the radiator and reject the heat to deep space by means of thermal radiation. As well, the system will allow for the recovery of deposited Carbon Dioxide. The UNT X-HAB 2021 team will create a model radiator and test its performance with simulated heat sources and sinks and extrapolate those data points to analyze for real world conditions.
Document ID
20210021757
Acquisition Source
Kennedy Space Center
Document Type
Other - FY21 Moon to Mars eXploration Systems and Habitation (M2M X-Hab) Academic Innovation Challenge Final Report
Authors
Travis Seaver
(University of North Texas Denton, Texas, United States)
Eric Lira
(University of North Texas Denton, Texas, United States)
Jesus De La Torre
(University of North Texas Denton, Texas, United States)
Anthony Pezzulli
(University of North Texas Denton, Texas, United States)
Balmore Giron
(University of North Texas Denton, Texas, United States)
Huseyin Bostanci
(University of North Texas Denton, Texas, United States)
Cable Kurwitz
(Texas A&M University )
Date Acquired
September 17, 2021
Publication Date
August 1, 2021
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
WBS: 089407
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Technical Management
No Preview Available