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Dual-bell altitude compensating nozzlesThe primary objective of this cold flow test effort was to assess the performance characteristics of dual bell nozzles and to obtain preliminary design criteria by testing a number of configurations. Characteristics of interest included low altitude performance, high altitude performance, and the flow transition process. In combination with this performance data, other factors such as cost, weight, fabricability, and vehicle related issues could then be traded to establish the feasibility of the concept.
Document ID
19940018584
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Horn, M.
(Rockwell International Corp. Canoga Park, CA, United States)
Fisher, S.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Publication Information
Publication: Pennsylvania State Univ., NASA Propulsion Engineering Research Center, Volume 2
Subject Category
Spacecraft Propulsion And Power
Accession Number
94N23057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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