Development of high burn rate propellant and testing in miniature rocket motor for control applications
For aerospace vehicles, notably missiles or satellites for attitude and divert control, impulsive thrusters are most desirable if they are quantized as exact instantaneous pulses available over and after extended periods of inactive storage. These thrusters operate for a few milliseconds (ms), typic...
| 发表在: | FirePhysChem |
|---|---|
| Main Authors: | , , |
| 格式: | 文件 |
| 语言: | 英语 |
| 出版: |
KeAi Communications Co. Ltd.
2024-06-01
|
| 主题: | |
| 在线阅读: | http://www.sciencedirect.com/science/article/pii/S2667134423000275 |