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Experimental Results for an Annular Aerospike with Differential ThrottlingMarshall Space Flight Center funded an internal study on Altitude Compensating Nozzles (ACN) for aerospike engines. The experimental hardware for the engine test is described in this viewgraph presentation, as well as the results of the experiment. The results include spike wall pressures, nozzle efficiency, and side force for four nozzle configurations.
Document ID
20040000846
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Ruf, Joseph H. (NASA Marshall Space Flight Center Huntsville, AL, United States)
McDaniels, David M. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
October 27, 2003
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: International Symposium on Liquid Space Propulsion
Location: Chattanooga, TN
Country: United States
Start Date: October 27, 2003
End Date: October 30, 2003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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