Space launch system - Revision history

Michel Lamontagne at 13:48, 26 August 2024

2024-08-26T13:48:06Z

← Older revision		Revision as of 14:48, 26 August 2024
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	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 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 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==		==Cost overruns==

RichardWSmith at 06:39, 24 August 2024

2024-08-24T06:39:08Z

← Older revision		Revision as of 07:39, 24 August 2024
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	==Cost overruns==		==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>		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]]		[[Category:Astronautics]]

RichardWSmith: Added section on high cost of use and cost overruns.

2024-08-24T06:38:40Z

Added section on high cost of use and cost overruns.

← Older revision		Revision as of 07:38, 24 August 2024
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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 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.

			==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>

	[[Category:Exploration Transport Systems]]		[[Category:Exploration Transport Systems]]
	[[Category:Astronautics]]		[[Category:Astronautics]]

Michel Lamontagne at 15:26, 2 September 2021

2021-09-02T15:26:57Z

← Older revision		Revision as of 16:26, 2 September 2021
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	[[Category:Exploration Transport Systems]]		[[Category:Exploration Transport Systems]]
			[[Category:Astronautics]]

Gladiator Decimus Meridius: /* Configuration */ Updated current expected SLS launch date.

2020-08-14T08:21:04Z

Configuration: Updated current expected SLS launch date.

← Older revision		Revision as of 09:21, 14 August 2020
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	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 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. ~~In March 2019~~ the first launch of the SLS was ~~still~~ scheduled for ~~2020~~.		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.

	[[Category:Exploration Transport Systems]]		[[Category:Exploration Transport Systems]]

Michel Lamontagne at 00:37, 6 August 2019

2019-08-06T00:37:42Z

← Older revision		Revision as of 01:37, 6 August 2019
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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==

Michel Lamontagne at 00:36, 6 August 2019

2019-08-06T00:36:52Z

← Older revision		Revision as of 01:36, 6 August 2019
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	==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 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).

Michel Lamontagne at 18:34, 10 May 2019

2019-05-10T18:34:03Z

← Older revision		Revision as of 19:34, 10 May 2019
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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.		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).

			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. In March 2019 the first launch of the SLS was still scheduled for 2020.

	[[Category:Exploration Transport Systems]]		[[Category:Exploration Transport Systems]]

Michel Lamontagne at 18:31, 10 May 2019

2019-05-10T18:31:56Z

← Older revision		Revision as of 19:31, 10 May 2019
Line 1:		Line 1:
	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. 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.		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.

	[[Category:Exploration Transport Systems]]		[[Category:Exploration Transport Systems]]

Jburk at 19:00, 17 December 2018

2018-12-17T19:00:24Z

← Older revision		Revision as of 20:00, 17 December 2018
Line 1:		Line 1:
	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. 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.		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. 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.

			[[Category:Exploration Transport Systems]]