Abstract
The influence of blocked spout on the performance of attitude control rocket motor was analyzed by numerical simulation and test. The results show that the motor can not generate required reverse thrust consistent to control signal when some spouts of the motor are blocked. When the ability of stabilizing the rocket axis is decreased, the delivery accuracy is reduced.
| Original language | English |
|---|---|
| Pages (from-to) | 101-104 |
| Number of pages | 4 |
| Journal | Guti Huojian Jishu/Journal of Solid Rocket Technology |
| Volume | 27 |
| Issue number | 2 |
| Publication status | Published - Jun 2004 |
Keywords
- Attitude control
- Numerical simulation
- Rocket engine
- Thrust measurement