Image:11D58Mengine.jpg
From The Space Library
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The close-cycle liquid fuel rocket engine 11D58M of TsKBEM development. This engine of 8.5 tons thrust uses oxygen and hydrocarbon fuel as propellant components. It was the world’s first engine to provide multiple in-flight firing.
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| Date/Time | Dimensions | User | Comment | |
|---|---|---|---|---|
| current | 20:29, 3 December 2015 | 870×1,272 (353 KB) | RobertG (Talk | contribs) | (The close-cycle liquid fuel rocket engine 11D58M of TsKBEM development. This engine of 8.5 tons thrust uses oxygen and hydrocarbon fuel as propellant components. It was the world’s first engine to provide multiple in-flight firing.) |
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