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Absorptive splitter for closely spaced supersonic engine air inlets PatentAbsorptive, nonreflecting barrier mounted between closely spaced jet engines on supersonic aircraft, for preventing shock wave interference
Document ID
19710006088
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Kastan, H. (Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 6, 2013
Publication Date
September 6, 1966
Subject Category
Propulsion Systems
Report/Patent Number
Patent Number: US-PATENT-3,270,990
Patent Number: NASA-CASE-XLA-02865
Patent Application Number: US-PATENT-APPL-SN-416946
Accession Number
71N15563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,270,990|NASA-CASE-XLA-02865
Patent Application
US-PATENT-APPL-SN-416946

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