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Handbook on Hypergolic Propellant Discharges and DisposalThe efficiency of all treatment methods formerly or currently used in treating chemical wastes is assessed with emphasis on the disposal of hypergolic propellants. Maximum focus is on the space shuttle propellants MMH and N2O4. Except for hydrogen peroxide oxidizers, all the propellants are nitrogen based and can be potentially reduced to valuable plant nutrients. In theory, all the propellants can be reduced to carbon, hydrogen, nitrogen, and oxygen, except of fuming nitric acid which contains a small amount of fluorine. Appendices cover: (1) a general design criteria for disposal ponds; (2) thermal aspects of reaction in dilute solution; (3) gas bubble growth, detachment, and rise (4) absorption scrubber fundamentals and descriptions; (5) separation of a propellant vapor from a helium stream by permeation; and (6) atmospheric emission limits.
Document ID
19810018759
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bowman, T. E.
(Florida Inst. of Tech. Melbourne, FL, United States)
Sivik, H. E.
(Florida Inst. of Tech. Melbourne, FL, United States)
Thomas, J. J.
(Florida Inst. of Tech. Melbourne, FL, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1977
Subject Category
Propellants And Fuels
Report/Patent Number
DD-MDD-41
NASA-CR-166826
Report Number: DD-MDD-41
Report Number: NASA-CR-166826
Accession Number
81N27297
Funding Number(s)
CONTRACT_GRANT: NAS10-8399
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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