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.
Program For Analyzing Designs Of Liquid-Propellant Rockets
NASA Tech Briefs ; 19 , 1
1995-01-01
Miscellaneous
No indication
English
Program for Analyzing Designs of Liquid-Propellant Rockets
Online Contents | 1995
NTRS | 1972
|NTIS | 1968
|Liquid propellant space rockets
NTRS | 1967
|NTIS | 1968
|