Space Launch System

Space Launch System
NASA's Space Launch System launching Artemis I with a bright trail of flame.
SLS Block 1 with the Orion spacecraft launching from Pad 39B
FunctionSuper heavy-lift launch vehicle
ManufacturerAerojet Rocketdyne
Northrop Grumman
Boeing
United Launch Alliance
Country of originUnited States
Project costUS$23.8 billion nominal[1]
Cost per launchOver US$2 billion excluding development (estimate) [note 1][2][3]: 23–24 [4][1]
Cost per yearUS$2.555 billion for FY 2021[5]
Size
HeightBlock 1 Crew: 322 ft (98 m)
Block 2 Cargo: 365 ft (111 m)
Diameter27.6 ft (8.4 m), Core stage [6]
16.7 ft (5.1 m), ICPS [7]
Mass5,750,000 lb (2,610 t)[8]
Stages2.5
Maximum thrust39,000,000 N (39 MN; 4,000 tf; 8,800,000 lbf) (Total first stage thrust.)[9]
Capacity
Payload to LEO [note 2]
Mass
  • Block 1: 209,000 lb (95 t)[11]
  • Block 1B: 231,000 lb (105 t)[12][13]
  • Block 2: 290,000 lb (130 t)[14]
Payload to trans-lunar injection
Mass
  • Block 1: > 59,500 lb (27 t)[15][16]
  • Block 1B Crew: 83,700 lb (38 t)
  • Block 1B Cargo: 92,500 lb (42 t)
  • Block 2 Crew: > 94,700 lb (43 t)
  • Block 2 Cargo: > 101,400 lb (46 t)
Associated rockets
Based on
Comparable
Launch history
StatusActive
Launch sitesKennedy Space Center, LC-39B
Total launches1
Success(es)1
First flight16 November 2022, 1:47:44 am EST (6:47:44 am UTC)[17]
Type of passengers/cargoOrion
Stage info
Boosters (Block 1, 1B)
No. boosters2 five-segment Solid Rocket Boosters
Height177 ft (54 m)[18]
Diameter12 ft (3.7 m)
Gross mass730 t (1,600,000 lb)[18]
Powered bySolid fuel
Maximum thrustSea level: 3,280,000 lbf (14.6 MN; 1,490 tf)
Vacuum: 3,600,000 lbf (16 MN; 1,600 tf)[19]
Total thrustSea level: 6,560,000 lbf (29.2 MN; 2,980 tf)
Vacuum: 7,200,000 lbf (32 MN; 3,300 tf)
Specific impulse269 s (2.64 km/s)
Burn time126 seconds
PropellantPBAN, APCP
First stage (Block 1, 1B, 2) – Core stage
Height212 ft (65 m)[20]
Diameter27.6 ft (8.4 m)
Empty mass187,990 lb (85 t)
Gross mass2,365,000 lb (1,073 t)
Powered by4 RS-25D/E
Maximum thrustSea level: 1,672,000 lbf (7.44 MN; 758 tf)[21]
Vacuum: 2,049,200 lbf (9.115 MN; 929.5 tf)[21]
Specific impulseSea level: 366 s (3.59 km/s)[21]
Vacuum: 452 s (4.43 km/s)[21]
Burn time480 seconds
PropellantLH2 / LOX
Second stage (Block 1) – ICPS
Height45 ft (13.7 m)[22]
Diameter16 ft (5 m) (LH2 tank) 10 ft (3.2 m) (LOX tank)[23]
Empty mass3,490 kg (7,690 lb)[24]
Gross mass32,066 kg (70,693 lb)
Powered by1 RL10B-2/C-2
Maximum thrust24,800 lbf (110.1 kN)
Specific impulse465.5 s (4.565 km/s)[25]
Burn time1125 seconds
PropellantLH2 / LOX
Second stage (Block 1B, Block 2) – Exploration Upper Stage
Height57 ft (17.3 m)[24]
Diameter28 ft (8.4 m) (LH2 tank) 18 ft (5.5 m) (LOX tank)[26]
Powered by4 RL10C-3, later 4 RL10C-X
Maximum thrust91,500 lbf (407.2 kN)
Burn time
  • 350 seconds (LEO ascent)
  • 925 seconds (TLI burn)
PropellantLH2 / LOX

The Space Launch System (SLS) is an American super heavy-lift expendable launch vehicle used by NASA. As the primary launch vehicle of the Artemis Moon landing program, SLS is designed to launch the crewed Orion spacecraft on a trans-lunar trajectory. The first SLS launch was the uncrewed Artemis 1, which took place on 16 November 2022.[27][17]

Development of SLS began in 2011, as a replacement for the retired Space Shuttle as well as the cancelled Ares I and Ares V launch vehicles.[28][29][30] As a Shuttle-derived vehicle, the SLS reuses hardware from the Shuttle program, including the solid rocket boosters and RS-25 first stage engines. A Congressionally mandated late 2016 launch was delayed by nearly 6 years.[31]

All Space Launch System flights are launched from Launch Complex 39B at the Kennedy Space Center in Florida. The first three SLS flights use the Block 1 configuration, comprising a core stage, extended Space Shuttle boosters developed for Ares I and the ICPS upper stage. An improved Block 1B configuration, with the Exploration Upper Stage, is planned to debut on the fourth flight; a further improved Block 2 configuration featuring new solid rocket boosters is planned to debut on the ninth flight.[32][33][34][35][11] After the launch of Artemis 4, NASA plans to transfer production and launch operations of SLS to Deep Space Transport LLC, a joint venture between Boeing and Northrop Grumman.[36]

  1. ^ a b c Cite error: The named reference doesnotdeny was invoked but never defined (see the help page).
  2. ^ Cite error: The named reference whitehouse was invoked but never defined (see the help page).
  3. ^ Cite error: The named reference OIG-22-023 was invoked but never defined (see the help page).
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  5. ^ Cite error: The named reference FY2021_SpendPlan was invoked but never defined (see the help page).
  6. ^ NASA (27 October 2021). "Space Launch System Core Stage". nasa.gov. Retrieved 19 November 2022.
  7. ^ NASA (18 November 2021). "Space Launch System Interim Cryogenic Propulsion Stage (ICPS)". nasa.gov. Retrieved 19 November 2022.
  8. ^ "SLS October 2015 Fact Sheet" (PDF).
  9. ^ NASA's Space Launch System Reference Guide v2.0 NASA pub. SLS-4071 NP-2022-08-65-MSFC. Page 5. August, 2022. Retrieved 2023-04-21.
  10. ^ "2018 draft factsheet of SLS capabilities" (PDF). NASA. 20 August 2018. Retrieved 24 August 2022.
  11. ^ a b Cite error: The named reference NASA 2018 Update was invoked but never defined (see the help page).
  12. ^ Cite error: The named reference slsfact-20171011 was invoked but never defined (see the help page).
  13. ^ Cite error: The named reference SLSBoeingPresentation2021 was invoked but never defined (see the help page).
  14. ^ Cite error: The named reference creech-2014 was invoked but never defined (see the help page).
  15. ^ Cite error: The named reference SLS_Overview was invoked but never defined (see the help page).
  16. ^ Cite error: The named reference SLS_Lift_Capacity was invoked but never defined (see the help page).
  17. ^ a b Cite error: The named reference nasa-blog-20221108 was invoked but never defined (see the help page).
  18. ^ a b Cite error: The named reference SRBSheet was invoked but never defined (see the help page).
  19. ^ Cite error: The named reference SLS Booster Development was invoked but never defined (see the help page).
  20. ^ Cite error: The named reference SLSCoreStageFactSheet was invoked but never defined (see the help page).
  21. ^ a b c d Cite error: The named reference RS-25 was invoked but never defined (see the help page).
  22. ^ Cite error: The named reference ICPS_ULA_Infographic_2021 was invoked but never defined (see the help page).
  23. ^ "Delta IV Launch Services User's Guide" (PDF). United Launch Alliance. Retrieved 13 April 2024.
  24. ^ a b Cite error: The named reference SLS_Specs_SFI was invoked but never defined (see the help page).
  25. ^ Cite error: The named reference RL10 was invoked but never defined (see the help page).
  26. ^ "1 year down, a galaxy to go". Boeing. Retrieved 13 April 2024.
  27. ^ Gebhardt, Chris; Burghardt, Thomas (16 November 2022). "SLS makes successful debut flight, sending Artemis I to the Moon". NASASpaceFlight.com. Retrieved 19 November 2022.
  28. ^ Cite error: The named reference senatebill was invoked but never defined (see the help page).
  29. ^ Cite error: The named reference SFN20110331 was invoked but never defined (see the help page).
  30. ^ Cite error: The named reference SR-20131125 was invoked but never defined (see the help page).
  31. ^ Cite error: The named reference PL-111-267 was invoked but never defined (see the help page).
  32. ^ Cite error: The named reference ASG-2014 was invoked but never defined (see the help page).
  33. ^ Cite error: The named reference nsf-20170406 was invoked but never defined (see the help page).
  34. ^ Cite error: The named reference NASA-20170512 was invoked but never defined (see the help page).
  35. ^ Cite error: The named reference NASA-20190815 was invoked but never defined (see the help page).
  36. ^ Potter, Sean Sean (27 July 2022). "NASA Prepares for Space Launch System Rocket Services Contract". NASA. Retrieved 10 August 2022.


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