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Automated Propellant BlendingAn automated propellant blending apparatus and method that uses closely metered addition of countersolvent to a binder solution with propellant particles dispersed therein to precisely control binder precipitation and particle aggregation is discussed. A profile of binder precipitation versus countersolvent-solvent ratio is established empirically and used in a computer algorithm to establish countersolvent addition parameters near the cloud point for controlling the transition of properties of the binder during agglomeration and finishing of the propellant composition particles. The system is remotely operated by computer for safety, reliability and improved product properties, and also increases product output.
Document ID
20010010200
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
Authors
Hohmann, Carl W.
(NASA Johnson Space Center Houston, TX United States)
Harrington, Douglas W.
(NASA Johnson Space Center Houston, TX United States)
Dutton, Maureen L.
(NASA Johnson Space Center Houston, TX United States)
Tipton, Billy Charles, Jr.
(NASA Johnson Space Center Houston, TX United States)
Bacak, James W.
(NASA Johnson Space Center Houston, TX United States)
Salazar, Frank
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
September 7, 2013
Publication Date
October 17, 2000
Subject Category
Propellants And Fuels
Report/Patent Number
Patent Number: NASA-Case-MSC-22757-2
Patent Application Number: US-Patent-Appl-SN-173609
Patent Application Number: US-Patent-Appl-SN-917581
Patent Number: US-Patent-6,132,536
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-MSC-22757-2|US-Patent-6,132,536
Patent Application
US-Patent-Appl-SN-173609|US-Patent-Appl-SN-917581
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