NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Employing ISRU Models to Improve Hardware DesignAn analytical model for hydrogen reduction of regolith was used to investigate the effects of several key variables on the energy and mass performance of reactors for a lunar in-situ resource utilization oxygen production plant. Reactor geometry, reaction time, number of reactors, heat recuperation, heat loss, and operating pressure were all studied to guide hardware designers who are developing future prototype reactors. The effects of heat recuperation where the incoming regolith is pre-heated by the hot spent regolith before transfer was also investigated for the first time. In general, longer reaction times per batch provide a lower overall energy, but also result in larger and heavier reactors. Three reactors with long heat-up times results in similar energy requirements as a two-reactor system with all other parameters the same. Three reactors with heat recuperation results in energy reductions of 20 to 40 percent compared to a three-reactor system with no heat recuperation. Increasing operating pressure can provide similar energy reductions as heat recuperation for the same reaction times.
Document ID
20110016034
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Linne, Diane L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2010
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA Paper-2010-800
E-17949
Report Number: AIAA Paper-2010-800
Report Number: E-17949
Meeting Information
Meeting: 48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Location: Orlando, FL
Country: United States
Start Date: January 4, 2010
End Date: January 7, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 387498.04.01.05.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available