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Problems of rocket exhaust plume interactions.Three dimensional interaction of multirocket vehicle exhaust jet plumes calculated, using finite difference analog to inviscid flow equations
Document ID
19680053844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dattorre, L.
Yoshihara, H.
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AGNE PUBLISHING, INC.,
Subject Category
Propulsion Systems
Meeting Information
Meeting: INTERNATIONAL SYMPOSIUM ON SPACE TECHNOLOGY AND SCIENCE
Location: TOKYO
Country: JAPAN
Start Date: May 15, 1967
End Date: May 22, 1967
Accession Number
68A34816
Distribution Limits
Public
Copyright
Other

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