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Liquid rocket propulsion dynamic flow modeling using the ROCETS engineering modules in the EASY5x environmentA report on the progress of porting the ROCETS (ROCket Engine Transient Simulator) into the EASY5x simulation environment is presented. Brief descriptions of each of the software systems, information regarding the actual port process, and examples comparing the results of the two systems are given. It is shown that EASY5x is a suitable environment for utilization of the ROCETS engineering modules, and that, for the example systems shown, EASY5x actually seems to give more accurate solutions than the straight ROCETS code.
Document ID
19930066312
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Follett, Randolph F. (NASA John C. Stennis Space Center Bay Saint Louis, MS, United States)
Taylor, Robert P. (Mississippi State Univ. Mississippi State, United States)
Nunez, Stephen C. (NASA Stennis Space Center Bay Saint Louis, MS, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA PAPER 93-2599
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: SAE, ASME, ASEE, AIAA
Accession Number
93A50309
Distribution Limits
Public
Copyright
Other

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