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Automated Propellant BlendingAn automated propellant blending apparatus and method uses closely metered addition of countersolvent to a binder solution with propellant particles dispersed therein to precisely control binder precipitation and particle aggregation. 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
19990046445
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
August 19, 2013
Publication Date
March 9, 1999
Subject Category
Propellants And Fuels
Report/Patent Number
Patent Number: NASA-Case-MSC-22757-1
Patent Application Number: US-Patent-Appl-SN-917581
Patent Number: US-Patent-5,879,079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-MSC-22757-1|US-Patent-5,879,079
Patent Application
US-Patent-Appl-SN-917581
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