File:Ssme schematic.svg
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Summary
[edit]DescriptionSsme schematic.svg |
English: A functional diagram showing the flow of propellant through an RS-25 engine. Very high flow rates are needed in the main combustion chamber, so the energy to achieve this is generated in upstream combustion "pre-burner" chambers that generate a partial burn to drive the high pressure turbopumps on both the fuel and oxidizer sides. Pressure feeding the preburners is maintained by the low-pressure turbopumps. Routing fuel through the nozzle serves to both cool the nozzle as well as pre-heat the fuel. |
Date | |
Source | Main Propulsion System (MPS) (PDF). Shuttle Press Kit.com. Boeing, NASA & United Space Alliance (6 October 1998). Retrieved on 7 December 2011. |
Author | Jkwchui |
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File history
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 04:44, 24 December 2011 | 800 × 571 (139 KB) | Jkwchui (talk | contribs) | (i) fixes lines in upper left; cleaned up lines (ii) added combustion zone to legend | |
10:33, 23 December 2011 | 800 × 571 (210 KB) | Jkwchui (talk | contribs) | (i) fixed overlapping lines (ii) added rendering (iii) added legend | ||
14:30, 21 December 2011 | 800 × 600 (31 KB) | Jkwchui (talk | contribs) |
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