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载人航天器参数对比
维基媒体列表条目 来自维基百科,自由的百科全书
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本条目针对现役及已退役的各型号载人航天器(包括载人飞船、航天飞机、空天飞机等)进行参数对比和记录。
各型号载人航天器对比
研发论证中 | |
现役 | |
已退役 | |
‡ | 上行/下行货物质量 |
§ | 载人(无人)飞行 [失败发射亦包含在内] |
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亚轨道载人飞行器对比
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脚注
- 其中包括两次亚轨道飞行,但不包括模拟航天器的测试。
- One uncrewed launch on Titan IIIC ahead of proposed use in MOL programme
- 不包括模拟航天器的测试。
- 虽然航天飞机理论上可搭乘8名以上的机组人员,但直到航天飞机退役之前,没有任何一次任务搭载过更多的宇航员。
- 翼展23.79米
- 无人飞行计数中包括两次失败发射。
- 在不穿戴舱内航天服的情况下可同时搭载3名宇航员,也可同时搭载2名着航天服的宇航员。
- Crewed flights include one launch failure - abort during third stage flight, recovered after suborbital flight
- Crewed flights include one launch failure (SAS (launch escape system) used ~70 seconds before planned liftoff due to fire on launch pad - crew survived)
- 最高可搭载7人,但国际空间站的商业航天运输任务至多将可搭载4名宇航员。
- Including uncrewed test around 2014
- Designed to land almost everywhere in the solar system
- Number of seats will be lower on early missions
- Does not include crewed atmospheric flights
- Does not include only-U.S.-recognized spaceflights
- Does not include atmospheric flights, or missions considered spaceflights by the US definition but not the FAI's definition
- 2 crew + 6 passengers
- Does not include crewed atmospheric flights
参见
参考资料
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