火箭详情
基本信息
| 名称 |
米诺陶 I |
| 全名 |
米诺陶 I |
| 家族 |
米诺陶 |
| 型号 |
|
| 制造商 |
Orbital Sciences Corporation |
规格参数
| 长度 |
19.21 m |
| 直径 |
1.67 m |
| 最小级数 |
4 |
| 最大级数 |
5 |
| 起飞质量 |
36 t |
| 起飞推力 |
935 kN |
| LEO运力 |
580 kg |
| GTO运力 |
- kg |
| 首飞时间 |
2000-01-27 |
描述
The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The first and second stages, taken directly from decommissioned Minuteman missiles, are mated to the Orion third and fourth stages taken from the Pegasus XL air-launched rocket family. An optional hydrazine-powered fifth stage called HAPS can be used.The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. An optional hydrazine-powered fifth stage called HAPS can be used.