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Nozzle fabrication techniqueThis invention relates to techniques for fabricating hour glass throat or convergent divergent nozzle shapes, and more particularly to new and improved techniques for forming rocket nozzles from electrically conductive material and forming cooling channels in the wall thereof. The concept of positioning a block of electrically conductive material so that its axis is set at a predetermined skew angle with relation to a travelling electron discharge machine electrode and thereafter revolving the body about its own axis to generate a hyperbolic surface of revolution, either internal or external is novel. The method will generate a rocket nozzle which may be provided with cooling channels using the same control and positioning system. The configuration of the cooling channels so produced are unique and novel. Also the method is adaptable to nonmetallic material using analogous cutting tools, such as, water jet, laser, abrasive wire and hot wire.
Document ID
19880015300
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Wells, Dennis L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.71:MSC-21299-1
Patent Application Number: US-PATENT-APPL-SN-176587
Patent Number: NASA-CASE-MSC-21299-1
Report Number: NAS 1.71:MSC-21299-1
Accession Number
88N24684
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MSC-21299-1
Patent Application
US-PATENT-APPL-SN-176587
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