| タイトル | Electrothermal thruster diagnostics. Volume 2: Technical |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830025672 |
| 著者（英） | Jackson, B.; Zafran, S. |
| 著者所属（英） | TRW, Inc. |
| 発行日 | 1983-05-01 |
| 言語 | eng |
| 内容記述 | Test data taken with nitrogen, hydrogen, and ammonia propellants are presented over a wide range of operating conditions at thrust levels up to 225 mN (50 mlb). The design adaptation of a flight-qualified thruster for operation with gaseous propellant inlet is described. Post-test analysis includes evaluation of thruster performance and efficiency, and shows the effects of propellant contamination on an immersed heating element. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 83N33943
NASA-CR-168174-VOL-2
TRW-39152-6012-UE-00-VOL-2
NAS 1.26:168174-VOL-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/161628 |
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