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词条 Exploration Upper Stage
释义

  1. Development

  2. Role & comparable stages

  3. See also

  4. References

{{Infobox rocket stage
|name = Exploration Upper Stage
|image =
|caption =
|manufacturer = Boeing[1]
|country = US
|rockets = SLS Block 1B [2]
|height = not to exceed {{convert|60|ft|abbr=on|order=flip}}
|diameter = {{convert|8.4|m|abbr=on}}
|propmass = up to {{convert|285,000|lb|abbr=on|order=flip}}
|engines = 4 RL10C-3[3][4]
|thrust = {{convert|99,000|lbf|kN|abbr=on|order=flip|lk=out}}
|time =
|fuel = LOX/LH2
}}

The Exploration Upper Stage (EUS) is being developed as a large second stage for Block 1B of the Space Launch System (SLS), succeeding Block 1's Interim Cryogenic Propulsion Stage. It will be powered by four RL10C-3[4] engines burning LOX/LH2 to produce a total of {{convert|99,000|lbf|kN|abbr=on|order=flip|lk=out}} thrust. {{asof|February 2015}} the SLS Block 1B is baselined at 105 metric tons.[5] The EUS is expected to first fly on the Exploration Mission 3 launch of the SLS scheduled for 2023.[6]

Development

The Block 1 configuration of SLS will have the ability to insert 70 metric tons[7] into low Earth orbit (LEO) using Shuttle-derived 5-segment Solid Rocket Boosters and a core stage powered by four RS-25 engines. Its second stage, the ICPS, will be considered part of the 70 t payload and on EM-1 it will be placed, along with the Orion crew capsule, on a 1,800 km by -93 km suborbital trajectory to ensure safe disposal of the core stage. At apogee, the ICPS will perform an insertion burn to raise the perigee and put itself and Orion into a stable orbit, and will later perform a translunar injection burn to send the uncrewed Orion capsule on a circumlunar excursion.[8]

To improve on the 70 metric ton Block 1, NASA considered a Block 1A upgrade which would replace the Shuttle-heritage boosters with advanced solid or liquid boosters, and a Block 1B upgrade which would develop an improved second stage. This improved stage was originally named the Dual Use Upper Stage (DUUS, pronounced "duce")[9] but was later renamed the Exploration Upper Stage (EUS) due to DUUS sounding like a profanity in Japanese.[10]

Following concerns that the more powerful Block 1A boosters would have resulted in high acceleration during launch, which would have been unsuitable for the Orion crew vehicle and could have resulted in a costly redesign of the SLS core,[11] NASA announced in 2014 that it would proceed with development of Block 1B with the EUS before advanced boosters.[2] In April 2016 it was reported NASA has chosen to use a design based on four RL10-C3 engines for the EUS,[3] and in Oct 2016 NASA confirmed they had ordered 10 of the engines.[4]

Role & comparable stages

The EUS is to complete the SLS's ascent phase and then re-ignite to send its payload to destinations beyond low Earth orbit, similar in function to the 3rd stage on the Saturn V, the J-2 powered S-IVB but closer to the 2nd stage on the Saturn I, the S-IV in engine layout, as it contained a cluster of RL-10 engines and was likewise a 2nd stage on the vehicle stack.

The 2nd stage of the SLS Block 1B, the EUS, powered by a cluster of four RL10 engines will produce slightly more thrust than the Saturn I's six engined S-IV of the 1960s.

Prior to finalization of second stage options for the SLS Block 1B, a more powerful Earth Departure Stage was under development, which would have been powered by up to three of the much more powerful J-2X engines.[12] Technological development of the J-2X was expected to take considerably more time, so the EDS was dropped in favor of the EUS, which will use the already-developed RL10. According to NASA, the J-2X will be overpowered for the lunar and asteroid missions of the Block 1 and 1B SLS; its development has been put on hold (though not abandoned) until stages capable of transferring heavy payloads to Mars are required (currently expected in the 2030s).[13]

See also

  • Delta Cryogenic Second Stage
  • Earth Departure Stage

References

1. ^{{cite web|title=NASA, Boeing Finalize $2.8B SLS Core Stage Contract|url=http://www.spacenews.com/article/civil-space/41139nasa-boeing-finalize-28b-sls-core-stage-contract|website=SpaceNews.com|accessdate=July 25, 2014}}
2. ^{{cite web|title=NASA confirms EUS for SLS Block IB design and EM-2 flight|url=http://www.nasaspaceflight.com/2014/06/nasa-confirms-eus-sls-block-ib-design-em-2-flight/|website=NASASpaceflight.com|accessdate=July 25, 2014}}
3. ^{{cite web|last=Bergin|first=Chris|title=MSFC propose Aerojet Rocketdyne supply EUS engines|url=https://www.nasaspaceflight.com/2016/04/msfc-aerojet-rocketdyne-eus-engines/ |publisher=NASASpaceFlight|accessdate=April 8, 2016|date=April 7, 2016}}
4. ^[https://www.nasa.gov/exploration/systems/sls/proven-engine-packs-big-in-space-punch-for-nasa-s-sls-rocket.html Proven Engine Packs Big, In-Space Punch for NASA’s SLS Rocket. Oct 2016]
5. ^{{cite news|title=Advanced Boosters progress towards a solid future for SLS|url=http://www.nasaspaceflight.com/2015/02/advanced-boosters-towards-solid-future-sls/|accessdate=2015-03-12|publisher=NasaSpaceflight.com|date=February 20, 2015}}
6. ^{{cite news|title=NASA updates Lunar Gateway plans|url=https://www.nasaspaceflight.com/2018/09/nasa-lunar-gateway-plans/|accessdate=2018-10-05|publisher=NasaSpaceflight.com|date=2018-09-11}}
7. ^{{cite web|title=SLS|url=http://space.skyrocket.de/doc_lau/sls.htm|website=Gunter's Space Page|accessdate=July 25, 2014}}
8. ^{{cite web|title=Space Launch System Data Sheet|url=http://www.spacelaunchreport.com/sls0.html|website=SpaceLaunchReport.com|accessdate=July 25, 2014}}
9. ^{{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/|website=NASASpaceflight.com|accessdate=July 25, 2014}}
10. ^{{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/|website=NASA Spaceflight|accessdate=November 8, 2014}}
11. ^{{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/|website=NASA SpaceFlight|accessdate=2015-03-12}}
12. ^{{cite web|title=SLS Launch Vehicle specifications take shape as development continues|url=http://www.nasaspaceflight.com/2012/03/sls-specifications-take-shape-development-continues/|website=NASASpaceflight.com|accessdate=July 24, 2014}}
13. ^{{Cite web|url=http://aviationweek.com/awin/nasa-s-j-2x-engine-be-mothballed-after-testing|title=NASA’s J-2X Engine To Be Mothballed After Testing|website=aviationweek.com|access-date=2016-08-16}}
{{Upper stages}}{{Use American English|date=July 2014}}{{Use mdy dates|date=July 2014}}

4 : Spacecraft propulsion|Aerospace engineering|Space Launch System|Rocket stages

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