Falcon 9
From Wikipedia, the free encyclopedia
Falcon 9 sī chi̍t lūi nn̄g-tōaⁿ-sek hoat-siā ūn-kū (launch vehicle), sú-iōng káu lia̍p tē-it kai-tōaⁿ ian-jín, seng-sán kiam siat-kè-chiá sī SpaceX kong-si. 2015 nî té í-āu hông sú-iōng ê khoán-sek sī Falcon 9 Full Thrust.
Quick Facts Function, 生產商 ...
A Falcon 9 lifting off from LC-39A, carrying Demo-2 | |
Function | Orbital launch vehicle |
---|---|
生產商 | SpaceX |
Sán-tōe | United States |
Cost per launch | |
Size | |
高度 | |
直徑 | 3.7 m (12 ft)[3] |
質量 | |
Stages | 2 |
Capacity | |
Payload to Low Earth orbit (LEO) | |
軌道傾角 | 28.5° |
質量 | |
Payload to Geosynchronous transfer orbit (GTO) | |
軌道傾角 | 27.0° |
質量 | |
Payload to Mars transfer orbit | |
質量 | FT: 4 t (8,800 lb)[1] |
Associated rockets | |
衍生作品 | Falcon Heavy |
Launch history | |
Status |
|
Launch sites |
|
Total launches |
|
Success(es) |
|
Failure(s) |
1 (v1.1: CRS-7 in-flight) |
Partial failure(s) | 1 (v1.0: CRS-1)[9] |
Notable outcome(s) | 1 (FT: AMOS-6 pre-flight destruction) |
Landings | / attempts |
First flight | |
Last flight |
|
First stage | |
發動機 |
|
最大推力 | |
Specific impulse | |
Burn time | |
Propellant | LOX / RP-1 |
Second stage | |
發動機 |
|
最大推力 | |
Specific impulse | |
Burn time | |
Propellant | LOX / RP-1 |
Close
Falcon 9 hē-thóng ê tē-it tōaⁿ thang têng-ho̍k sú-iōng; siang kai-tōaⁿ lóng tàu lī-ēng e̍k-thé sng-sò͘ kap RP-1 jiân-liāu thui-sak ê hóe-chìⁿ ian-jín.