| タイトル | Preliminary performance characterizations of an engineering model multipropellant resistojet for space station application |
| 著者（英） | Morren, W. Earl; Haag, Thomas W.; Hay, Stuart S.; Sovey, James S. |
| 著者所属（英） | NASA Lewis Research Center; Purdue Univ. |
| 発行日 | 1987-06-01 |
| 言語 | eng |
| 内容記述 | Presented are the results of a program to describe the operational characteristics of an engineering model multipropellant resistojet for application as an auxiliary propulsion system for the space station. Performance was measured on hydrogen, helium, methane, water (steam), nitrogen, air, argon, and carbon dioxide. Thrust levels ranged from 109 to 355 mN, power levels ranged from 167 to 506 W, and specific impulse values ranged from 93 to 385 sec, depending on the propellant, chamber pressure, and heater current level selected. Detailed thermal maps of the heater and heat exchanger were also obtained for operation with carbon dioxide. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 87A50197
AIAA PAPER 87-2120 |
| 権利 | Copyright |
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