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|fuel = LOX / RP-1 <!--fuel used in stage/boosters, required-->
|fuel = LOX / RP-1 <!--fuel used in stage/boosters, required-->
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}}
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** [[Falcon 9 v1.0|v1.0]]
** [[Falcon 9 v1.1|v1.1]]
** [[Falcon 9 Full Thrust|"Full Thrust" v1.2]]
** Block 4
| group4 = Dibatalkan
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| group4 = Wahana dapat digunakan ulang
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* [[Daftar pendorong tahap pertama Falcon 9|Pendorong tahap pertama]]
** [[Pendorong Falcon 9 B1046|B1046]]
** [[Pendorong Falcon 9 B1048|B1048]]
** [[Pendorong Falcon 9 B1056|B1056]]
* Kapsul kargo
** [[SpaceX Dragon C106|C106]]
** [[SpaceX Dragon C108|C108]]

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|below = <nowiki>*</nowiki> denotes unflown vehicles or engines, and future missions or sites. † denotes failed missions, destroyed vehicles, and abandoned sites.
}}
}}

Revisi per 25 Juni 2020 08.40

Falcon 9 Full Thrust
[[Berkas:|270px|Peluncuran pertama Falcon 9 v1.2 (Full Thrust) yang membawa muatan satelit Orbcomm di Cape Canaveral Air Force Station]]
Peluncuran pertama Falcon 9 v1.2 (Full Thrust) yang membawa muatan satelit Orbcomm di Cape Canaveral Air Force Station
Fungsi Orbital medium-lift launch vehicle
Produsen SpaceX
Negara asal Amerika Serikat
Biaya per peluncuran (2024) $62M (2016),[1] $50M (2018)[2]
Ukuran
Tinggi 71 m (233 ft) with payload fairing[3]
Diameter 366 m (1.201 ft)[4]
Massa 549,000 kg (1.210,338 pon)[4]
Tingkatan 2
Kapasitas
Muatan menuju OBR (28.5°)
Massa
  • Expendable: 22,800 kg (50,27 pon),[1] 15.600 kg (34.400 pon) when landing
  • PAF structural limit: 10,886 kg (24,00 pon)[3]
Muatan menuju OGS (27°)
Massa
  • Expendable: 8,300 kg (18,30 pon)[1]
  • Reusable: 5.500 kg (12.100 pon)[1]
Muatan menuju Mars
Massa4,020 kg (8,86 pon)[1]
Roket terkait
Keluarga Falcon 9
Derivatif Falcon Heavy
Roket sejenis
Sejarah peluncuran
Status Active
Tempat peluncuran
Total peluncuran 67[5]
Keberhasilan
peluncuran 		67
Lainnya 1 (destroyed before launch)
Penerbangan perdana 22 December 2015
Penerbangan terakhir 4 June 2020 (Starlink-7)
Muatan
Tingkat First
Mesin9 Merlin 1D
Daya dorongSea level: 7,607 kN (1.710 lbf)[4]
Vacuum: 8,227 kN (1.850 lbf)[4]
Impuls spesifikSea level: 282 seconds[6][dated info]
Vacuum: 311 seconds[6][dated info]
Durasi pembakaran162 seconds[4]
Bahan bakarSubcooled LOX / Chilled RP-1[7]
Tingkat Second
Mesin1 Merlin 1D Vacuum
Daya dorong934 kN (210.000 lbf)[4]
Impuls spesifik348 seconds[4]
Durasi pembakaran397 seconds[4]
Bahan bakarLOX / RP-1
  1. ^ a b c d e "Capabilities & Services (2016)". SpaceX. 2012-11-28. Diakses tanggal 3 May 2016. 
  2. ^ Baylor, Michael (17 May 2018). "With Block 5, SpaceX to increase launch cadence and lower prices". NASASpaceFlight.com. Diakses tanggal 24 May 2018. 
  3. ^ a b "Falcon 9 Launch Vehicle Payload User's Guide" (PDF). 21 October 2015. Diarsipkan dari versi asli (PDF) tanggal 14 March 2017. Diakses tanggal 29 November 2015. 
  4. ^ a b c d e f g h "Falcon 9". SpaceX. 2012-11-16. Diakses tanggal 30 April 2016. 
  5. ^ Krebs, Gunter. "Falcon-9". Gunter's Space Page. Diakses tanggal 7 November 2018. 
  6. ^ a b "Falcon 9". SpaceX. 2012-11-16. Diarsipkan dari versi asli tanggal 1 May 2013. Diakses tanggal 29 September 2013. 
  7. ^ Elon Musk [@elonmusk] (2015-12-17). "-340 F in this case. Deep cryo increases density and amplifies rocket performance. First time anyone has gone this low for O2. [RP-1 chilled] from 70F to 20 F" (Tweet). Diakses tanggal 19 December 2015 – via Twitter. 
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