Difference between revisions of "Space launch system"
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| − | NASA's Space Launch System (SLS) is a super-heavy-lift launch vehicle designed to support human exploration activities beyond Earth orbit. Begun in 2011, the program is a hold-over from NASA's Constellation Program, which was canceled in 2010. | + | [[Earth|NASA's]] Space Launch System (SLS) is a super-heavy-lift launch vehicle designed to support human exploration activities beyond Earth orbit. Begun in 2011, the program is a hold-over from NASA's Constellation Program, which was canceled in 2010. |
| − | == Configuration == | + | ==Configuration== |
| − | Leveraging NASA investments in Space Shuttle and Constellation Program hardware, the SLS launch vehicle comprises an 8.4-meter-diameter core stage, which is the same diameter as the Space Shuttle external tank. The core stage is flanked by two five-segment solid rocket boosters modified from the four-segment SRBs used on Shuttle. Core stage main propulsion will be provided by four RS-25E Space Shuttle main engines repurposed for the SLS application. The upper stage comprises a Delta (IV) Cryogenic Second Stage (DCSS) with a single RL10 engine, called the Interim Cryogenic Propulsion Stage (ICPS). The ICPS will eventually be replaced by a four-engine upper stage Advanced Cryogenic Evolved Stage (ACES). | + | Leveraging [[NASA]] investments in Space Shuttle and Constellation Program hardware, the SLS launch vehicle comprises an 8.4-meter-diameter core stage, which is the same diameter as the Space Shuttle external tank. The core stage is flanked by two five-segment solid rocket boosters modified from the four-segment SRBs used on Shuttle. Core stage main propulsion will be provided by four RS-25E Space Shuttle main engines repurposed for the SLS application. The upper stage comprises a Delta (IV) Cryogenic Second Stage (DCSS) with a single RL10 engine, called the Interim Cryogenic Propulsion Stage (ICPS). The ICPS will eventually be replaced by a four-engine upper stage Advanced Cryogenic Evolved Stage (ACES). |
| − | The initial capability of the "Block 1A" vehicle (scheduled to launch by mid-2020) is 70,000 kg to low-Earth orbit. later versions of the vehicle are slated to carry up to 105,000 kg (Block 1B) and 130,000 kg (Block 2). The first launch of SLS will be an unmanned Orion spacecraft, which will perform autonomous maneuvers around the Moon (including a Distant Retrograde Orbit) before returning to Earth for splashdown. | + | The initial capability of the "Block 1A" vehicle (scheduled to launch by mid-2020) is 70,000 kg to low-Earth orbit. later versions of the vehicle are slated to carry up to 105,000 kg (Block 1B) and 130,000 kg (Block 2). |
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| + | The first launch of SLS will be an unmanned Orion spacecraft, which will perform autonomous maneuvers around the Moon (including a Distant Retrograde Orbit) before returning to Earth for splashdown. As of August 2020 the first launch of the SLS was scheduled for November of 2021. The first unmanned launch finally took place on 16 November 2022. The first crewed flight is planed for 2025. | ||
| + | |||
| + | ==Cost overruns== | ||
| + | The program has a long history of cost overruns. Considering the cheaper commercial launch services, some consider it to be unaffordable for long term space exploration.<ref>https://www.space.com/nasa-sls-rocket-artemis-moon-plans-unaffordable-gao-report</ref> | ||
| + | |||
| + | ==References== | ||
[[Category:Exploration Transport Systems]] | [[Category:Exploration Transport Systems]] | ||
| + | [[Category:Astronautics]] | ||
Latest revision as of 06:48, 26 August 2024
NASA's Space Launch System (SLS) is a super-heavy-lift launch vehicle designed to support human exploration activities beyond Earth orbit. Begun in 2011, the program is a hold-over from NASA's Constellation Program, which was canceled in 2010.
Configuration
Leveraging NASA investments in Space Shuttle and Constellation Program hardware, the SLS launch vehicle comprises an 8.4-meter-diameter core stage, which is the same diameter as the Space Shuttle external tank. The core stage is flanked by two five-segment solid rocket boosters modified from the four-segment SRBs used on Shuttle. Core stage main propulsion will be provided by four RS-25E Space Shuttle main engines repurposed for the SLS application. The upper stage comprises a Delta (IV) Cryogenic Second Stage (DCSS) with a single RL10 engine, called the Interim Cryogenic Propulsion Stage (ICPS). The ICPS will eventually be replaced by a four-engine upper stage Advanced Cryogenic Evolved Stage (ACES).
The initial capability of the "Block 1A" vehicle (scheduled to launch by mid-2020) is 70,000 kg to low-Earth orbit. later versions of the vehicle are slated to carry up to 105,000 kg (Block 1B) and 130,000 kg (Block 2).
The first launch of SLS will be an unmanned Orion spacecraft, which will perform autonomous maneuvers around the Moon (including a Distant Retrograde Orbit) before returning to Earth for splashdown. As of August 2020 the first launch of the SLS was scheduled for November of 2021. The first unmanned launch finally took place on 16 November 2022. The first crewed flight is planed for 2025.
Cost overruns
The program has a long history of cost overruns. Considering the cheaper commercial launch services, some consider it to be unaffordable for long term space exploration.[1]
