
Space Launch System
NASA’s Space Launch System is the backbone for a permanent human presence in deep space, for multiple missions to the moon and eventually to Mars and beyond.
NASA's Space Launch System (SLS) provides a critical heavy-lift capability built to rigorous human-rated safety standards to carry people and cargo back to the moon – this time to stay – and on to Mars.
SLS will launch larger payloads farther in our solar system, faster than ever before possible. It will be the most powerful rocket ever built, enabling diverse exploration, science and security missions. SLS is also the world’s only super heavy rocket capable of safely transporting astronauts to deep space with major payloads like landers, habitats and Gateway elements.
Boeing is the prime contractor for the design, development, test and production of the launch vehicle core stage, as well as development of the flight avionics suite.
The first test flight, Artemis I, will carry an uncrewed Orion space capsule to the moon to test the performance of the integrated system. SLS also will carry 13 small satellites, each about the size of a shoebox, that will be deployed in deep space.
Additional missions are planned with this configuration as the even more powerful Block 1B version of the rocket is designed and built. This follow-on, evolved two-stage configuration will provide a lift capability of more than 105 metric tons, using the Boeing-built Exploration Upper Stage. Boeing has delivered flight hardware for the first Artemis mission and is producing flight hardware for both the second and third missions.
NASA is Boeing's customer for the Space Launch System, the largest rocket ever built, which will take humans and crew well beyond low-Earth orbit and into deep space.
The Boeing SLS Program is managed out of the company’s Space and Launch division in Huntsville, Ala., and employs Boeing’s workforce in Huntsville, at NASA’s Michoud Assembly Facility in New Orleans, and at other Boeing sites and with suppliers across the country. The Boeing Exploration Launch Systems office supports NASA on strategy and policy for Space Exploration programs procured by the NASA Marshall Space Flight Center.
Stage | Core Stage | Block 1 Interim Cryogenic Propulsion Stage | Block 1B Exploration Upper Stage |
---|---|---|---|
Length | 212 ft (64.6 m) | 38.0 ft (11.58 m) | 57.6 ft (11.5 m) |
Diameter | 27.6 ft (8.4 m) | 16.4 ft (5.0 m) | 27.6 ft (8.4 m) |
Propellant Weight | 2,175,423 lbs | 63,206 lbs | 278,000 lbs |
Empty Weight | 188,000 lbs | 7,700 lbs | 33,156 lbs |
Material | Aluminum 2219 | Aluminum | Aluminum |
Engines | 4 RS-25 | 1 RL 10-C1 | 4 RL-10 |
Thrust per Engine | 512,000 lbf | 24,854 lbf | 24,340 lbf |
Total Thrust at Max Power | 2.2 million lbf (1.09%) | 24,854 lbf (1.00%) | 97,360 lbf (1.00%) |
Fuel | Liquid Hydrogen | Liquid Hydrogen | Liquid Hydrogen |
Oxidizer | Liquid Oxygen | Liquid Oxygen | Liquid Oxygen |
Want to learn more about SLS and its role in Boeing's space exploration business? Visit Watch U.S. Fly for more information.