Exploration Upper Stage: Difference between revisions
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NASA will develop the EUS to increase SLS performance beyond Block 1 specifications. The improved upper stage was originally named the Dual Use Upper Stage (DUUS, pronounced "duce")<ref name=nsfpdr>{{cite web |title=SLS prepares for PDR – Evolution eyes Dual-Use Upper Stage |url=http://www.nasaspaceflight.com/2013/06/sls-pdr-evolved-rocket-dual-upper-stage/ |publisher=NASASpaceflight.com |date=June 2013 |access-date=July 25, 2014}}</ref> but was later renamed the Exploration Upper Stage (EUS) due to DUUS sounding like a profanity in Japanese.<ref>{{cite web |last1=Bergin |first1=Chris |title=SLS positioning for ARRM and Europa missions |url=http://www.nasaspaceflight.com/2014/03/sls-positioning-arrm-europa-missions/ |publisher=NASASpaceflight.com |date=March 28, 2014 |access-date=November 8, 2014}}</ref> |
NASA will develop the EUS to increase SLS performance beyond Block 1 specifications. The improved upper stage was originally named the Dual Use Upper Stage (DUUS, pronounced "duce")<ref name=nsfpdr>{{cite web |title=SLS prepares for PDR – Evolution eyes Dual-Use Upper Stage |url=http://www.nasaspaceflight.com/2013/06/sls-pdr-evolved-rocket-dual-upper-stage/ |publisher=NASASpaceflight.com |date=June 2013 |access-date=July 25, 2014}}</ref> but was later renamed the Exploration Upper Stage (EUS) due to DUUS sounding like a profanity in Japanese.<ref>{{cite web |last1=Bergin |first1=Chris |title=SLS positioning for ARRM and Europa missions |url=http://www.nasaspaceflight.com/2014/03/sls-positioning-arrm-europa-missions/ |publisher=NASASpaceflight.com |date=March 28, 2014 |access-date=November 8, 2014}}</ref> |
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In 2014, NASA announced that it would proceed with development of Block 1B with the EUS<ref>{{cite web |last1=Bergin |first1=Chris |title=Wind Tunnel testing conducted on SLS configurations, including Block 1B |url=http://www.nasaspaceflight.com/2012/07/wind-tunnel-testing-sls-configurations-block-1b/ |publisher=NASASpaceFlight.com |date=July 30, 2012 |access-date=2015-03-12}}</ref> and would use it on EM-2.<ref name=nsfe/> In April 2016, it was reported that NASA has chosen to use a design based on four [[RL10|RL10-C3]] engines for the EUS,<ref name="RL10_Variants">{{cite web | archive-date=November 7, 2021 | archive-url=https://web.archive.org/web/20211107110702/https://www.rocket.com/space/liquid-engines/rl10-engine | url=https://www.rocket.com/space/liquid-engines/rl10-engine | title=RL10 Engine | accessdate=November 18, 2021 | url-status=live | website=Aerojet Rocketdyne}}</ref> and in October 2016 NASA confirmed they had ordered 10 of the engines.<ref name=" |
In 2014, NASA announced that it would proceed with development of Block 1B with the EUS<ref>{{cite web |last1=Bergin |first1=Chris |title=Wind Tunnel testing conducted on SLS configurations, including Block 1B |url=http://www.nasaspaceflight.com/2012/07/wind-tunnel-testing-sls-configurations-block-1b/ |publisher=NASASpaceFlight.com |date=July 30, 2012 |access-date=2015-03-12}}</ref> and would use it on EM-2.<ref name=nsfe/> In April 2016, it was reported that NASA has chosen to use a design based on four [[RL10|RL10-C3]] engines for the EUS,<ref name="RL10_Variants">{{cite web | archive-date=November 7, 2021 | archive-url=https://web.archive.org/web/20211107110702/https://www.rocket.com/space/liquid-engines/rl10-engine | url=https://www.rocket.com/space/liquid-engines/rl10-engine | title=RL10 Engine | accessdate=November 18, 2021 | url-status=live | website=Aerojet Rocketdyne}}</ref> and in October 2016 NASA confirmed they had ordered 10 of the engines.<ref name="RL10C3_Order_2016">{{cite web | url=https://www.nasa.gov/exploration/systems/sls/proven-engine-packs-big-in-space-punch-for-nasa-s-sls-rocket.html | title=Proven Engine Packs Big, In-Space Punch for NASA’s SLS Rocket | publisher=NASA | date=October 21, 2016 | accessdate=18 November 2021}}</ref> |
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In 2018, it was decided to optimise EUS for payload to lunar missions, by using smaller tanks.<ref name=NSF-2021-Feb>[https://www.nasaspaceflight.com/2021/02/nasa-completes-exploration-upper-stage-cdr-focuses-new-office-on-sls-block-1b-development/ ''NASA completes Exploration Upper Stage CDR, focuses new office on SLS Block 1B development'']. Feb 2021.</ref> |
In 2018, it was decided to optimise EUS for payload to lunar missions, by using smaller tanks.<ref name=NSF-2021-Feb>[https://www.nasaspaceflight.com/2021/02/nasa-completes-exploration-upper-stage-cdr-focuses-new-office-on-sls-block-1b-development/ ''NASA completes Exploration Upper Stage CDR, focuses new office on SLS Block 1B development'']. Feb 2021.</ref> |
Revision as of 08:19, 18 November 2021
![]() 2020 Design of the Exploration Upper Stage | |
Manufacturer | Boeing[1] |
---|---|
Country of origin | Vereinigte Staaten |
Used on | SLS Block 1B and Block 2[2] |
General characteristics | |
Height | not to exceed 18 m (59 ft) |
Diameter | 8.4 m (28 ft) |
Propellant mass | up to 129,000 kg (284,000 lb) |
Engine details | |
Powered by | 4 RL10C-3[3] |
Maximum thrust | 433.1 kN (97,360 lbf) |
Propellant | LOX / LH2 |
The Exploration Upper Stage (EUS) is being developed as a large second stage for Block 1B and Block 2 of the Space Launch System (SLS), succeeding Block 1's Interim Cryogenic Propulsion Stage. It will be powered by four RL10C-3 engines burning liquid oxygen and liquid hydrogen to produce a total thrust of 433.1 kN (97,360 lbf). As of October 2017[update], the SLS Block 1B will have a payload capacity to low Earth orbit of 105 t (116 short tons; 231,000 lb) and Block 2 will have a payload capacity of 130 t (140 short tons; 290,000 lb).[2] The EUS is expected to first fly on Artemis IV in March 2026.[4]
Development
The Block 1 configuration of SLS will have a core stage powered by four RS-25 engines, two Space Shuttle-derived five-segment solid rocket boosters, and an Interim Cryogenic Propulsion Stage (ICPS) upper stage.[5][6]
NASA will develop the EUS to increase SLS performance beyond Block 1 specifications. The improved upper stage was originally named the Dual Use Upper Stage (DUUS, pronounced "duce")[7] but was later renamed the Exploration Upper Stage (EUS) due to DUUS sounding like a profanity in Japanese.[8]
In 2014, NASA announced that it would proceed with development of Block 1B with the EUS[9] and would use it on EM-2.[10] In April 2016, it was reported that NASA has chosen to use a design based on four RL10-C3 engines for the EUS,[3] and in October 2016 NASA confirmed they had ordered 10 of the engines.[11]
In 2018, it was decided to optimise EUS for payload to lunar missions, by using smaller tanks.[12]
By February 2020, the development contract for EUS had been delayed, and NASA was planning to use ICPS for the first three launches of SLS.[13]
Boeing announced on 21 December 2020 that the Exploration Upper Stage (EUS) of the SLS completed a critical design review (CDR) with NASA. That review confirmed the design of the EUS, allowing Boeing to proceed with development of the stage, including hardware fabrication.[14]
Funding History
Fiscal year | Nominal
(millions) |
In 2021[15](millions) |
---|---|---|
2016 | $77.0 | $84.8 |
2017 | $300.0[16] | $324.3 |
2018 | $300.0[17] | $316.5 |
2019 | $150.0[18] | $155.1 |
2020 | $300.0 | $303.9 |
2021 | $400.0[note 1] | $400.0 |
Total: 2016–2021 | $1,527.0 | $1,584.6 |
Cost concerns and alternatives
Due to the possible cost of EUS (about US$800 million each), NASA invited proposals for alternatives, but in May 2019 rejected Blue Origin's proposal.[19] NASA ordered eight EUSs from Boeing.[19]
See also
Notes
- ^ The FY2021 spending plan indicates that this is for "Block 1B (non-add) (including EUS)"
References
- ^ "NASA, Boeing Finalize US$2.8 billion SLS Core Stage Contract". SpaceNews. 4 July 2014. Archived from the original on 27 July 2014. Retrieved 25 July 2014.
- ^ a b "SLS October 2017 Fact Sheet" (PDF). Archived (PDF) from the original on 1 November 2021. Retrieved 18 November 2021.
- ^ a b "RL10 Engine". Aerojet Rocketdyne. Archived from the original on 7 November 2021. Retrieved 18 November 2021.
- ^ Sloss, Philip (17 February 2021). "NASA completes Exploration Upper Stage CDR, focuses new office on SLS Block 1B development". NASASpaceFlight.com. Retrieved 17 November 2021.
The recent GAO-21-105 audit noted that the Artemis 4 mission that would debut Block 1B and EUS is forecast to launch in March 2026.
- ^ "SLS". Gunter's Space Page. Retrieved 25 July 2014.
- ^ "Space Launch System Data Sheet". SpaceLaunchReport.com. Retrieved 25 July 2014.
- ^ "SLS prepares for PDR – Evolution eyes Dual-Use Upper Stage". NASASpaceflight.com. June 2013. Retrieved 25 July 2014.
- ^ Bergin, Chris (28 March 2014). "SLS positioning for ARRM and Europa missions". NASASpaceflight.com. Retrieved 8 November 2014.
- ^ Bergin, Chris (30 July 2012). "Wind Tunnel testing conducted on SLS configurations, including Block 1B". NASASpaceFlight.com. Retrieved 12 March 2015.
- ^ Cite error: The named reference
nsfe
was invoked but never defined (see the help page). - ^ "Proven Engine Packs Big, In-Space Punch for NASA's SLS Rocket". NASA. 21 October 2016. Retrieved 18 November 2021.
- ^ NASA completes Exploration Upper Stage CDR, focuses new office on SLS Block 1B development. Feb 2021.
- ^ Upper Stage RL10s arrive at Stennis for upcoming SLS launches. February 2020.
- ^ "SLS Exploration Upper Stage passes review". SpaceNews. 22 December 2020. Retrieved 22 December 2020.
- ^ "NASA FY20 Inflation Tables – to be utilized in FY21". NASA. p. Inflation Table. Retrieved 11 October 2021.
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- ^ "NASA outlines plan for 2024 lunar landing". SpaceNews. 1 May 2019. Archived from the original on 30 September 2021. Retrieved 15 May 2019.
- ^ Berger, Eric (20 May 2019). "NASA's full Artemis plan revealed: 37 launches and a lunar outpost". Ars Technica. Archived from the original on 23 May 2019. Retrieved 20 May 2019.
- ^ Sloss, Philip. "Amid competing priorities, Boeing redesigns NASA SLS Exploration Upper Stage". NASASpaceFlight.com. Archived from the original on 7 August 2020. Retrieved 25 July 2020.
- ^ a b NASA rejects Blue Origin's offer of a cheaper upper stage for the SLS rocket May 2019