SLS (Block-1) [NASA]
SLS (Block-2) [NASA]
The SLS (Space Launch System) is NASA's planned heavy lift rocket replacing the cancelled Ares-5 concept.
The SLS will be designed to carry the Orion Multi-Purpose Crew Vehicle, as well as important cargo, equipment and science experiments to Earth's orbit and destinations beyond. Additionally, the SLS will serve as a back up for commercial and international partner transportation services to the International Space Station.
The rocket concept is also called in-line SD-HLV (Shuttle derived - Heavy Lift Launch Vehicle) as it uses many parts of Shuttle heritage. It will consist of two 5-segmented solid rocket boosters (SRB) derived from the 4-segmented SRBs of the Shuttle. The core is also derived from the Shuttle 8.4 m diameter external tank and will be powered by versions of the Shuttle's SSME engines. Initially it will use RS-25D engines left over from the shuttle program, while later they will be replaced by expendable versions called RS-25E. The early developent flights will use three engines, while later versions can also use five engines for increased performance.
The initial two flights will use the 5-segmented SRB, but for later versions, the boosters will be competed based on performance requirements and affordability considerations. Both Advanced Composite Boosters (ACBs) and Liquid Rocket Boosters (LRBs) are under consideration.
The first flight will use an interim cryogenic upper stage (iCPS) derived from the 5 m version of the Delta-4 upper stage featuring the RL10B-2 engine.
Further flights will use the EUS upper stage, which is powered by four RL10C-3 engines.
On the later Block 2 version, an upper stage using the J-2X engine of Saturn-5 heritage will be used for high energy missions.
The first developmental flight of a SLS Block-1 iCPS version is targeted for 2018. The second flight will use the upgraded SLS Block-1B EUS version.
|Version||Strap-On||Stage 1||Stage 2|
|SLS (Block-1)||2 × SRB-5||4 × RS-25D||-|
|SLS (Block-1) iCPS||2 × SRB-5||4 × RS-25D||iCPS / RL10B-2|
|SLS (Block-1A)||2 × advanced Booster||4 × RS-25D/E||-|
|SLS (Block-1A) EUS||2 × advanced Booster||4 × RS-25D/E||EUS / 4 × RL10C-3|
|SLS (Block-1B)||2 × SRB-5||4 × RS-25D/E||-|
|SLS (Block-1B) EUS||2 × SRB-5||4 × RS-25D/E||EUS / 4 × RL10C-3|
|SLS (Block-2)||2 × advanced Booster||4 or 5 × RS-25E||Upper Stage / 2 × J-2X|
|SLS (Block 1)||70000||-||-||-||-||-|
|SLS (Block 1) iCPS||28000|
|SLS (Block 1A)||105000||-||-||-||-||-|
|SLS (Block 1A) EUS|
|SLS (Block 1B)||105000||-||-||-||-||-|
|SLS (Block 1B) EUS||45000|
|SLS (Block 2)||130000|
No: TNo: Serial: Type: Fai Date LS Payload
none planned: 1 1 SLS (Block 1) iCPS xx.xx.2018 CC LC-39B Orion EM1 / BioSentinel / CuSP / LunaH-Map / Lunar-Flashlight / Lunar-IceCube / NEA-Scout / SkyFire / EQUULEUS / OMOTENASHI / ArgoMoon / 3 cubesats 2 1 SLS (Block 1B) EUS xx.xx.2021 CC LC-39B Orion EM2 Launch sites: CC = NASA John F. Kennedy Space Center, Cape Canaveral, Florida, USA