| タイトル | Program For Analyzing Designs Of Liquid-Propellant Rockets |
| 著者（英） | Giuliani, James E.; Walker, Dick; Nguyen, Thong V.; Johnson, Curtis W.; Muss, Jeff A.; Klem, Mark D. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1995-01-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | MECHANICS |
| レポートNO | 95B10031
LEW-15114 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/306049 |
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