Wikipedia

User:LemonSlushie/Drafts/Starship (Launch Vehicle)

< User:LemonSlushie | Drafts
Starship
Has use
ManufacturerSpaceX
Country of originUnited States
Cost per launchUS$2 million (aspirational) [2]
Size
Height122 m (400 ft)[3][4]
Diameter9 m (30 ft)[5]
Mass5,000,000 kg (11,000,000 lb) (with payload) [6][4]
Stages2
Capacity
Payload to LEO
Mass100,000 kg (220,000 lb)[7]
Volume1,100 m3 (39,000 cu ft)[7]
Associated rockets
FamilySpaceX launch vehicles
Comparable
Launch history
StatusIn development
Launch sites
Total launches0
Success(es)0
Failure(s)0
Partial failure(s)0
Landings0
First stage – Super Heavy
Height72 m (236 ft) [4][7]
Diameter9 m (30 ft) [7]
Empty mass180,000 kg (400,000 lb) (estimated)[6]
Gross mass3,580,000 kg (7,890,000 lb) [6][7][8]
Propellant mass3,400,000 kg (7,500,000 lb) [7]
Powered by~28 Raptor [9]
Maximum thrust65,000 kN (15,000,000 lbf) [10]
Specific impulse330 s (3.2 km/s) [11]
PropellantSubcooled CH
4 / LOX [5]
Second stage – Starship
Height50 m (160 ft) [7]
Diameter9 m (30 ft) [7]
Empty mass120,000 kg (260,000 lb) [6]
Gross mass1,320,000 kg (2,910,000 lb) [6][7][8]
Propellant mass1,200,000 kg (2,600,000 lb) [7]
Powered by6 Raptor [5]
Maximum thrustc. 12,000 kN (2,700,000 lbf) [5]
Specific impulse380 s (3.7 km/s) (vacuum) [12]
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  1. ↑ Cite error: The named reference cnbc20200901 was used but no text was provided for refs named (see the help page).
  2. ↑ Cite error: The named reference sdc20191106 was used but no text was provided for refs named (see the help page).
  3. ↑ "Archived copy". Archived from the original on 12 August 2020. Retrieved 15 August 2020.{{cite web}}: CS1 maint: archived copy as title (link)
  4. ↑ 4.0 4.1 4.2 @elonmusk (16 March 2020). "Slight booster length increase to 70 m, so 120 m for whole system. Liftoff mass ~5000 mT" (Tweet) – via Twitter.
  5. ↑ 5.0 5.1 5.2 5.3 Cite error: The named reference sx20190930 was used but no text was provided for refs named (see the help page).
  6. ↑ 6.0 6.1 6.2 6.3 6.4 @elonmusk (26 September 2019). "Mk1 ship is around 200 tons dry and 1400 tons wet, but aiming for 120 by Mk4 or Mk5. Total stack mass with max payload is 5000 tons" (Tweet) – via Twitter.
  7. ↑ 7.00 7.01 7.02 7.03 7.04 7.05 7.06 7.07 7.08 7.09 Cite error: The named reference sx20200524 was used but no text was provided for refs named (see the help page).
  8. ↑ 8.0 8.1 Lawler, Richard. "SpaceX's plan for in-orbit Starship refueling: a second Starship". engadget.com. Archived from the original on 2 October 2019. Retrieved 29 September 2019.
  9. ↑ Cite error: The named reference sn20200901 was used but no text was provided for refs named (see the help page).
  10. ↑ "Archived copy". Archived from the original on 2 September 2020. Retrieved 1 September 2020.{{cite web}}: CS1 maint: archived copy as title (link)
  11. ↑ Cite error: The named reference musk20170929 was used but no text was provided for refs named (see the help page).
  12. ↑ Musk, Elon (17 September 2018). First Private Passenger on Lunar BFR Mission. SpaceX. Retrieved 18 September 2018 – via YouTube.
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