| タイトル | Hydrazine engine plume contamination mapping |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760018257 |
| 著者（英） | Chirivella, J. E. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1975-10-01 |
| 言語 | eng |
| 内容記述 | Instrumentation for the measurement of plume exhaust specie deposition rates were developed and demonstrated. The instruments, two sets of quartz crystal microbalances, were designed for low temperature operation in the back flow and variable temperature operation in the core flow regions of an exhaust plume. These quartz crystal microbalances performed nominally, and measurements of exhaust specie deposition rates for 8400 number of pulses for a 0.1-lb monopropellant thruster are reported. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 76N25345
NASA-CR-147936
AD-A018729
AFRPL-TR-75-16 |
| 権利 | No Copyright |
