火箭详情
基本信息
| 名称 |
电子号 |
| 全名 |
电子号 |
| 家族 |
未知 |
| 型号 |
|
| 制造商 |
火箭实验室 |
规格参数
| 长度 |
18 m |
| 直径 |
1.2 m |
| 最小级数 |
2 |
| 最大级数 |
3 |
| 起飞质量 |
13 t |
| 起飞推力 |
162 kN |
| LEO运力 |
300 kg |
| GTO运力 |
- kg |
| 首飞时间 |
2017-05-25 |
描述
Electron is a two-stage orbital expendable launch vehicle (with an optional third stage) developed by the American aerospace company Rocket Lab. Electron is a small-lift launch vehicle designed to launch small satellites and cubesats to sun-synchronous orbit and low earth orbit. The Electron is the first orbital class rocket to use electric-pump-fed engines, powered by the 9 Rutherford engines on the first stage. It is also used as a suborbital testbed (called HASTE) for hypersonics research.
