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The Exploration Upper Stage (EUS) was a planned rocket stage for NASA's Space Launch System (SLS) during 2013 to 2026. It was intended for use on the proposed SLS Block 1B and Block 2 configurations, replacing the Interim Cryogenic Propulsion Stage (ICPS) used on the Block 1 variant. The EUS was designed to be powered by four RL10C-3 engines burning…
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Exploration Upper Stage | Burn time | 1,275 seconds | 1.00 | infobox |
| Exploration Upper Stage | Country of origin | United States | 1.00 | infobox |
| Exploration Upper Stage | Diameter | LH2 tank: 8.4 m (28 ft) | 1.00 | infobox |
| Exploration Upper Stage | Diameter | LOX tank: 5.5 m (18 ft) | 1.00 | infobox |
| Exploration Upper Stage | Empty mass | 14,110 kg (31,110 lb) | 1.00 | infobox |
| Exploration Upper Stage | Height | 17.3 m (57 ft) | 1.00 | infobox |
| Exploration Upper Stage | Manufacturer | Boeing | 1.00 | infobox |
| Exploration Upper Stage | Maximum thrust | 433.1 kN (97,360 lbf) | 1.00 | infobox |
| Exploration Upper Stage | Powered by | 4 × RL10C-3 | 1.00 | infobox |
| Exploration Upper Stage | Propellant | LH2 / LOX | 1.00 | infobox |
| Exploration Upper Stage | Propellant mass | 129,000 kg (284,000 lb) | 1.00 | infobox |
| Exploration Upper Stage | Specific impulse | 460.1 s (4.512 km/s) | 1.00 | infobox |
| Exploration Upper Stage | Used on | Space Launch System (Block 1B/2) | 1.00 | infobox |
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