Abstract
The solid propellant impulsive thruster performance was analyzed from the plume image with a high-speed digital camera. With the high-speed photography the impulsive thruster exhaust plume characteristics can show not only the ignition and thrust capability, but also the energy efficiency of the thruster. It is concluded that the impulsive thruster performance can be improved by using the plume image analysis, especially with the complement of combination of image analysis and thrust and/or pressure analysis.
| Original language | English |
|---|---|
| Pages (from-to) | 477-480 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 25 |
| Issue number | 5 |
| Publication status | Published - Oct 2004 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- Exhaust flame
- High speed photography
- Image analysis
- Impulse rocket engine
- Solid propellant
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