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 engines burning liquid oxygen and liquid hydrogen to produce a total of 440 kN (99,000 lbf) thrust. As of February 2015, the SLS Block 1B will provide thrust of 105 metric tons (231,000 lb). The EUS is expected to first fly on Artemis IV.

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dbo:abstract
  • Exploration Upper Stage (EUS) sedang dikembangkan sebagai tahap kedua untuk Blok 1B dan Blok 2 dari Space Launch System (SLS), menggantikan Blok 1 dari Interim Cryogenic Propulsion Stage. Ini akan didukung oleh empat mesin pembakaran LOX / LH2 RL 10 untuk menghasilkan total daya dorong 440 kN (99.000 lbf). EUS ini diharapkan untuk terbang pada peluncuran kedua SLS dijadwalkan untuk 2021. (in)
  • 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 engines burning liquid oxygen and liquid hydrogen to produce a total of 440 kN (99,000 lbf) thrust. As of February 2015, the SLS Block 1B will provide thrust of 105 metric tons (231,000 lb). The EUS is expected to first fly on Artemis IV. (en)
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  • Diagram of the Exploration Upper Stage (en)
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  • not to exceed (en)
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  • 300 (xsd:integer)
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  • Exploration Upper Stage (en)
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  • up to (en)
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  • SLS Block 1B (en)
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  • Exploration Upper Stage (EUS) sedang dikembangkan sebagai tahap kedua untuk Blok 1B dan Blok 2 dari Space Launch System (SLS), menggantikan Blok 1 dari Interim Cryogenic Propulsion Stage. Ini akan didukung oleh empat mesin pembakaran LOX / LH2 RL 10 untuk menghasilkan total daya dorong 440 kN (99.000 lbf). EUS ini diharapkan untuk terbang pada peluncuran kedua SLS dijadwalkan untuk 2021. (in)
  • 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 engines burning liquid oxygen and liquid hydrogen to produce a total of 440 kN (99,000 lbf) thrust. As of February 2015, the SLS Block 1B will provide thrust of 105 metric tons (231,000 lb). The EUS is expected to first fly on Artemis IV. (en)
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  • Exploration Upper Stage (en)
  • Exploration Upper Stage (in)
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