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| 报告编号 | NASA-CR-134068, CASD-NAS-73-020 |
| 来源ID | NTRS_Document_ID: 19740004417 |
| RCS jet-flow field interaction effects on the aerodynamics of the space shuttle orbiter | |
| Rausch, J. R.; Roberge, A. M. | |
| 英文摘要 | A study was conducted to determine the external effects caused by operation of the reaction control system during entry of the space shuttle orbiter. The effects of jet plume-external flow interactions were emphasized. Force data were obtained for the basic airframe characteristics plus induced effects when the reaction control system is operating. Resulting control amplification and/or coupling were derived and their effects on the aerodynamic stability and control of the orbiter and the reaction control system thrust were determined. |
| 英文关键词 | ATTITUDE CONTROL JET THRUST REENTRY PHYSICS SPACE SHUTTLE ORBITERS SPACECRAFT GUIDANCE AERODYNAMIC CHARACTERISTICS SPACECRAFT PERFORMANCE SPACECRAFT STABILITY |
| 出版年 | 1973 |
| 报告类型 | Technical Report |
| 语种 | 英语 |
| 国家 | 美国 |
| URL | http://hdl.handle.net/2060/19740004417 |
| 资源类型 | 科技报告 |
| 条目标识符 | http://119.78.100.177/qdio/handle/2XILL650/258539 |
| 推荐引用方式 GB/T 7714 | Rausch, J. R.,Roberge, A. M.. RCS jet-flow field interaction effects on the aerodynamics of the space shuttle orbiter,1973. |
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