NASA NTRS · 19950065190
Program For Analyzing Designs Of Liquid-Propellant Rockets
Abstract
Rocket Combustor Interactive Design Computer Methodology (ROCCID) computer program provides standardized methodology, using state-of-art codes and procedures, for analysis of combustion performance and stability of liquid-propellant rocket engine. Provides combustion analyst with software tool to analyze existing combustor design (point-analysis option), or design high-performance, stable combustor, given set of input design requirements (point-design option). Written in ANSI FORTRAN 77 and VAX FORTRAN.
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Klem, Mark D., Muss, Jeff A., Nguyen, Thong V., Walker, Dick, Johnson, Curtis W., Giuliani, James E.. 1995-01-01. Program For Analyzing Designs Of Liquid-Propellant Rockets. https://ntrs.nasa.gov/citations/19950065190
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