米诺陶 IV HAPS | STP S-26
发射信息
| 任务代号： | 2010-062 |
| 发射状态： | 发射成功 |
| 发射服务商： | Orbital Sciences Corporation |
| 火箭型号： | 米诺陶 IV HAPS |
| 火箭家族： | 米诺陶 |
| 任务名称： | STP S-26 |
| 任务类型： | Dedicated Rideshare |
| 发射地点： | 太平洋太空港综合体，阿拉斯加，美国 |
| 发射工位： | 发射台1 |
| 轨道类型： | 近地轨道 |
任务详情
The third Minotaur IV launch, which was also known as STP-S26, deployed eight payloads (STPSat-2, RAX, O/OREOS, FASTSAT, NanoSail-D2, FalconSat-5, Sara-Lily (FASTRAC 1), Emma (FASTRAC 2)). STP-S26 was intended to extend previous standard interface development efforts, implementing a number of capabilities aimed at enabling responsive access to space for small experimental satellites and payloads.
运营机构
未知
火箭详情
基本信息
| 名称 | 米诺陶 IV |
| 全名 | 米诺陶 IV HAPS |
| 家族 | 米诺陶 |
| 型号 | HAPS |
| 制造商 | Orbital Sciences Corporation |
规格参数
| 长度 | 23.9 m |
| 直径 | 2.35 m |
| 最小级数 | 5 |
| 最大级数 | 5 |
| 起飞质量 | 86 t |
| 起飞推力 | 2200 kN |
| LEO运力 | 1750 kg |
| GTO运力 | 0 kg |
| 首飞时间 | 2010-11-20 |
描述
The Minotaur IV HAPS launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeeper missiles. A fourth stage, the Orion-38, is taken from the Pegasus family of air-launched rockets. A fifth stage, consisting of a hydrazine-powered motor called HAPS, increases orbital insertion accuracy and allows additional orbital maneuvering.
发射场详情
| 发射场名称 | 太平洋太空港综合体，阿拉斯加，美国 |
| 发射工位 | 发射台1 |
| 国家 | 美国 |
| 经纬度 | 57.435833, -152.337778 |
