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More About N2O-Based Propulsion and Breathable-Gas SystemsA concept was evaluated of using nitrous oxide as (1) a monopropellant in thrusters for space suits and spacecraft and (2) a source of breathable gas inside space suits and spacecraft, both by exploiting the controlled decomposition of N2O into N2 and O2. Relative to one prior monopropellant hydrazine, N2O is much less toxic, yet offers comparable performance. N2O can be stored safely as a liquid at room temperature and unlike another prior monopropellant hydrogen peroxide does not decompose spontaneously. A prototype N2O-based thruster has been demonstrated. It has also been proposed to harness N2O-based thrusters for generating electric power and to use the N2 + O2 decomposition product as a breathable gas. Because of the high performance, safety, and ease of handling of N2O, it can be expected to be economically attractive to equip future spacecraft and space suits with N2O-based thrusters and breathable-gas systems.
Document ID
20100024434
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Zubrin, Robert
(Pioneer Astronautics Lakewood, CO, United States)
Mungas, Greg
(Pioneer Astronautics Lakewood, CO, United States)
Caviezel, K. Mark
(Pioneer Astronautics Lakewood, CO, United States)
Date Acquired
August 24, 2013
Publication Date
July 1, 2010
Publication Information
Publication: NASA Tech Briefs, July 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
MSC-23707-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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