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Enriched Storable Oxidizers for Rocket EnginesThe name "enriched storable oxidizers" (ESOs) has been coined for a family of optimized mixtures of between two and four oxidizer fluids. For most applications, the constituents of these mixtures would be nitrogen tetroxide (N2O4), nitrous oxide (N2O), and nitrogen dioxide (NO2); in some applications, the mixtures might include inhibited red fuming nitric acid [IRFN (which consists of red fuming nitric acid to which some hydrogen fluoride is added to reduce its corrosive effect]. The optimum proportions of these constituents would be different for different applications. ESOs were originally proposed for use in spacecraft and launch-rocket propulsion systems: ESOs could be especially useful in advanced spacecraft propulsion systems that could operate in multiple modes. ESOs might also be useful in special terrestrial applications that could include ramjet and scramjet aircraft engines.
Document ID
20100019583
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Sackheim, R. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Herdy, J. R., Jr.
(Qualis Corp. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Publication Information
Publication: NASA Tech Briefs, May 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MFS-32407-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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