Khoàⁿ "Falcon 9"--ê goân-sí lōe-iông

{{Infobox rocket
| name           = Falcon 9
| logo           = Falcon 9 logo.svg
| logo_alt       = Logo of the Falcon 9
| image          = SpaceX Demo-2 Launch (NHQ202005300044) (cropped).jpg
| alt            = Ground-level view of a Falcon 9 lifting off from its launch pad
| caption        = A Falcon 9 lifting off from [[Kennedy Space Center Launch Complex 39A|LC-39A]], carrying [[Demo-2]]

| function       = [[Orbital spaceflight|Orbital]] [[launch vehicle]]
| manufacturer   = [[SpaceX]]
| country-origin = [[United States]]
| cpl            = {{plainlist|
* New: US$67 million (2022)<ref name=spacex-capabilities/>
* Reused: US$50 million? (2019)<ref name="Starship2021">{{cite web|url=https://spacenews.com/spacex-targets-2021-commercial-starship-launch/|title=SpaceX targets 2021 commercial Starship launch|date=28 June 2019|access-date=30 June 2019|archive-date=28 August 2019|archive-url=http://webarchive.loc.gov/all/20190828053242/https://spacenews.com/spacex%2Dtargets%2D2021%2Dcommercial%2Dstarship%2Dlaunch/|url-status=live}}</ref>
}}
| height         = {{plainlist|
* '''[[Falcon 9 Full Thrust|FT]]''': {{cvt|70|m}}<ref name=falcon9-2015/>
* '''v1.1''': {{cvt|68.4|m}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt|54.9|m}}<ref name=falcon9-2010/>
}}
| diameter       = {{cvt|3.7|m}}<ref name=falcon9-2015/>
| mass = {{plainlist|
* '''FT''': {{cvt |549 |t|lb}}<ref name=falcon9-2015/>
* '''v1.1''': {{cvt|506|t|lb}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt|333|t|lb}}<ref name=falcon9-2010/>
}}
| stages         = 2
| capacities =
  {{Infobox rocket/payload
  |location      = [[Low Earth orbit]] (LEO)
  |inclination   = 28.5°
  |kilos         = {{plainlist|
* '''FT''': {{cvt |22.8 | t| lb}}<ref name=spacex-capabilities/> Expended <br/>{{cvt|16.7| t| lb}}<ref>{{cite news |last1=Clark |first1=Stephen |title=SpaceX launch sets record for Falcon 9 payload mass – Spaceflight Now |url=https://spaceflightnow.com/2022/08/27/falcon-9-starlink-4-23-live-coverage/ |access-date=28 August 2022 |publisher=Spaceflight Now / Pole Star Publications Ltd}}</ref> when landing on [[Autonomous spaceport drone ship|ASDS]]
* '''v1.1''': {{cvt|13.1| t| lb}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt|10.4| t| lb}}<ref name=falcon9-2010/>
    }}
  }}
  {{Infobox rocket/payload
  |location      = [[Geosynchronous transfer orbit]] (GTO)
  |inclination   = 27.0°
  |kilos         = {{plainlist|
* '''FT''': {{cvt|8.3| t| lb}} Expended <br/>{{cvt|5.5| t| lb}} when landing on [[Autonomous spaceport drone ship|ASDS]]<ref name=spacex-capabilities/><br/>{{cvt|3.5| t| lb}} when RTLS<ref>{{cite web |url=https://spaceflightnow.com/2018/12/17/air-force-requirements-will-keep-spacex-from-recovering-falcon-9-booster-after-gps-launch/|title=Air Force requirements will keep SpaceX from landing Falcon 9 booster after GPS launch|publisher=Spaceflight Now|access-date=17 May 2019|archive-url=https://web.archive.org/web/20190520110216/https://spaceflightnow.com/2018/12/17/air-force-requirements-will-keep-spacex-from-recovering-falcon-9-booster-after-gps-launch/|archive-date=20 May 2019|url-status=live}}</ref>
* '''v1.1''': {{cvt|4.8| t| lb}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt|4.5| t| lb}}<ref name=falcon9-2010/>
    }}
  }}
  {{Infobox rocket/payload
  |location      = [[Heliocentric orbit|Mars transfer orbit]]
  |kilos         = '''FT''': {{cvt|4| t| lb}}<ref name=spacex-capabilities/>
  }}

|derivatives     = [[Falcon Heavy]]
|status          = {{plainlist|
* '''[[Falcon 9 Full Thrust Block 5|FT Block 5]]''': Active<ref>{{cite web|url=https://www.popularmechanics.com/space/rockets/a20152543/spacex-test-fire-new-falcon-9-block-5/|title=SpaceX Test-Fires New Falcon 9 Block 5 Rocket Ahead of Maiden Flight (Updated)|first=Robin|last=Seemangal|date=4 May 2018|publisher=Popular Mechanics|access-date=2 February 2019|archive-url=https://web.archive.org/web/20190407102712/https://www.popularmechanics.com/space/rockets/a20152543/spacex-test-fire-new-falcon-9-block-5/|archive-date=7 April 2019|url-status=live}}</ref>
* '''FT Block 4''': Retired
* '''FT Block 3''': Retired
* '''v1.1''': Retired
* '''v1.0''': Retired
}}
|sites           = {{plainlist|
* [[Cape Canaveral Air Force Station|Cape Canaveral]], [[Cape Canaveral Space Launch Complex 40|SLC-40]]
* [[Kennedy Space Center]], [[Kennedy Space Center Launch Complex 39A|LC-39A]]
* [[Vandenberg Air Force Base|Vandenberg]], [[Vandenberg Space Launch Complex 4|SLC-4E]]
}}
|launches        = {{flatlist|
* [[List of Falcon 9 and Falcon Heavy launches|{{Falcon rocket statistics|F9launch}}]]
** '''FT''': {{Falcon rocket statistics|F9FTlaunch}}
** '''v1.1''': 15
** '''v1.0''': 5
}}
|success         = {{flatlist|
* {{Falcon rocket statistics|F9success}}
** '''FT''': {{Falcon rocket statistics|F9FTsuccess}}
** '''v1.1''': 14
** '''v1.0''': 4
}}
|fail            = 1 <br>('''v1.1''': [[SpaceX CRS-7|CRS-7]] in-flight)
|partial         = 1 ('''v1.0''': [[SpaceX CRS-1|CRS-1]])<ref name="sn20121011">{{cite news |url=http://spacenews.com/orbcomm-craft-launched-by-falcon-9-falls-out-of-orbit/ |title=Orbcomm Craft Launched by Falcon 9 Falls out of Orbit |quote=[[Orbcomm]] requested that SpaceX carry one of their small satellites (weighing a few hundred pounds, versus Dragon at over 12,000 pounds)... The higher the orbit, the more test data [Orbcomm] can gather, so they requested that we attempt to restart and raise altitude. NASA agreed to allow that, but only on condition that there be substantial propellant reserves, since the orbit would be close to the [[International Space Station]]. It is important to appreciate that [[Orbcomm]] understood from the beginning that the orbit-raising maneuver was tentative. They accepted that there was a high risk of their satellite remaining at the Dragon insertion orbit... |last=de Selding |first=Peter B. |publisher=Space News |date=15 October 2012 |access-date=15 October 2012 |archive-date=12 May 2015 |archive-url=https://archive.today/20150512125706/http://spacenews.com/orbcomm-craft-launched-by-falcon-9-falls-out-of-orbit/ |url-status=live }}</ref>
|other_outcome   = 1 ('''FT''': [[AMOS-6]] pre-flight destruction)
|landings        = {{Falcon rocket statistics|F9Landingsuccess}} / {{Falcon rocket statistics|F9Landingattempt}} attempts
|first           = {{plainlist|
* '''FT Block 5''': 11 May 2018 <br/>([[Bangabandhu Satellite-1]])
* '''FT''': 22 December 2015 <br/>([[Falcon 9 flight 20|OG2 Flight 2]])<ref name="nasaspaceflight.com">{{cite web|url=http://www.nasaspaceflight.com/2015/12/spacex-rtf-core-return-attempt-og2/|title=SpaceX returns to flight with OG2, nails historic core return|last1=Graham|first1=William|publisher=NASASpaceFlight|access-date=22 December 2015|date=21 December 2015|quote=The launch also marked the first flight of the Falcon 9 Full Thrust, internally known only as the "Upgraded Falcon 9"|archive-url=https://web.archive.org/web/20151222224303/http://www.nasaspaceflight.com/2015/12/spacex-rtf-core-return-attempt-og2/|archive-date=22 December 2015|url-status=live}}</ref>
* '''v1.1''': 29 September 2013<br/>[[CASSIOPE]]<ref name=nsfdc20130929>{{cite web|url=http://www.nasaspaceflight.com/2013/09/spacex-debut-falcon-9-v1-1-cassiope-launch/|title=SpaceX successfully launches debut Falcon 9 v1.1|last=Graham|first=Will|publisher=NASASpaceFlight|access-date=29 September 2013|date=29 September 2013|archive-url=https://web.archive.org/web/20130929164727/http://www.nasaspaceflight.com/2013/09/spacex-debut-falcon-9-v1-1-cassiope-launch/|archive-date=29 September 2013|url-status=live}}</ref>
* '''v1.0''': 4 June 2010<br/>[[Dragon Spacecraft Qualification Unit|(Dragon COTS Demo 1)]]<ref name="MSDB"/>
}}
|last            = {{plainlist|
* '''FT Block 4''': 29 June 2018 ([[SpaceX CRS-15]])
* '''v1.1''': 17 January 2016<br/>([[Jason-3]])
* '''v1.0''': 1 March 2013<br/>([[SpaceX CRS-2]])
}}
|stagedata = 
  {{Infobox rocket/stage
  |type          = stage
  |stageno       = First
  |name          = <!-- name of the stage optional -->
  |length        = <!-- length of a single stage in metres, use {{cvt|LENGTH|m}}, optional -->
  |diameter      = <!-- diameter of a single stage in metres, use {{cvt|DIAMETER|m}}, optional -->
  |empty         = <!-- empty mass of a single stage in kilograms, use {{cvt|EMPTYMASS|kg}}, optional -->
  |gross         = <!-- gross (fuelled) mass of a single stage, use {{cvt|GROSSMASS|kg}}, optional -->
  |propmass      = <!-- propellant mass carried by a single stage in kilograms, use {{cvt|PROPMASS|kg}}, optional -->
  |engines       = {{plainlist|
* '''FT Block 5''': 9 [[SpaceX Merlin|Merlin 1D]]+ (maximum thrust)
* '''FT''': 9 [[SpaceX Merlin|Merlin 1D]]+
* '''v1.1''': 9 [[SpaceX Merlin|Merlin 1D]]
* '''v1.0''': 9 [[SpaceX Merlin|Merlin 1C]]
}}
  |thrust        = {{plainlist|
* '''FT <small>(late 2016)</small>''': {{cvt|7.6| MN| t-f lbf}}<ref name=falcon9-2016/>
* '''FT''': {{cvt|6.8| MN| t-f lbf}}<ref name=falcon9-2015/>
* '''v1.1''': {{cvt|5.9| MN| t-f lbf}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt|4.9| MN| t-f lbf}}<ref name=falcon9-2010/>
}}
  |SI            = {{plainlist|
* '''v1.1'''
** '''Sea level''': {{cvt|282|isp|km/s}}<ref name=falcon9-v1.1-si>{{cite web|title=Falcon 9|url=http://www.spacex.com/falcon9.php|publisher=SpaceX|access-date=29 September 2013 |archive-url=https://web.archive.org/web/20130501002858/http://www.spacex.com/falcon9.php|archive-date=1 May 2013|date=16 November 2012}}</ref>
** '''Vacuum''': {{cvt|311|isp|km/s}}<ref name=falcon9-v1.1-si/>
* '''v1.0'''
** '''Sea level''': {{cvt|275|isp|km/s}}<ref name=falcon9-2010/>
** '''Vacuum''': {{cvt|304|isp|km/s}}<ref name=falcon9-2010/>
}}
  |burntime      = {{plainlist|
* '''FT''': 162 seconds<ref name=falcon9-2015/>
* '''v1.1''': 180 seconds<ref name=falcon9-2013/>
* '''v1.0''': 170 seconds
}}
  |fuel          =[[LOX]] / [[RP-1]]
  }}
  {{Infobox rocket/stage
  |type          = stage
  |stageno       = Second
  |length        = <!-- length of a single stage in metres, use {{cvt|LENGTH|m}}, optional -->
  |diameter      = <!-- diameter of a single stage in metres, use {{cvt|DIAMETER|m}}, optional -->
  |empty         = <!-- empty mass of a single stage in kilograms, use {{cvt|EMPTYMASS|kg}}, optional -->
  |gross         = <!-- gross (fuelled) mass of a single stage, use {{cvt|GROSSMASS|kg}}, optional -->
  |propmass      = <!-- propellant mass carried by a single stage in kilograms, use {{cvt|PROPMASS|kg}}, optional -->
  |engines       = {{plainlist|
* '''FT''': 1 [[Merlin 1D Vacuum]]+
* '''v1.1''': 1 Merlin 1D Vacuum
* '''v1.0''': 1 [[Merlin 1C Vacuum]]
}}
  |thrust        = {{plainlist|
* '''FT''': {{cvt| 934| kN| t-f lbf}}<ref name=falcon9-2015/>
* '''v1.1''': {{cvt| 801| kN| t-f lbf}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt| 617| kN| t-f lbf}}<ref name=falcon9-2010/>
}}
  |SI            = {{plainlist|
* '''FT''': {{cvt| 348| isp| km/s}}<ref name=falcon9-2015/>
* '''v1.1''': {{cvt| 340| isp| km/s}}<ref name=falcon9-2013/>
* '''v1.0''': {{cvt| 342| isp| km/s}}<ref name="SpaceX March 10, 2009"/>
}}
  |burntime      = {{plainlist|
* '''FT''': 397 seconds<ref name=falcon9-2015/>
* '''v1.1''': 375 seconds<ref name=falcon9-2013/>
* '''v1.0''': 345 seconds<ref name=falcon9-2010/>
}}
  |fuel          = LOX / RP-1
  }}
}}

'''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]].

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]].

==Tsù-kái==
{{reflist|2}}

{{stub}}

[[Category:Hóe-chìⁿ]]
[[Lūi-pia̍t:SpaceX]]