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The YF-73 was China's first successful cryogenic liquid hydrogen fuel and liquid oxygen oxidizer gimballed engine. It was used on the Long March 3 H8 third stage, running on the simple gas generator cycle and with a thrust of 44.15 kilonewtons (9,930 lbf). It had four hinge mounted nozzles that gimbaled each on one axis to supply thrust vector control…
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hydrogen oxygen engine first thrust yf-75 used gas generator liquid march lbf restart long h8 third stage cycle 44 15
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| YF-73 | Associated LV | Long March 3 | 1.00 | infobox |
| YF-73 | Burn time | 800 seconds (13 min) | 1.00 | infobox |
| YF-73 | Chamber | 4 | 1.00 | infobox |
| YF-73 | Chamber pressure | 2,590 kPa (25.9 bar) | 1.00 | infobox |
| YF-73 | Country of origin | China | 1.00 | infobox |
| YF-73 | Cycle | Gas-generator | 1.00 | infobox |
| YF-73 | Designer | Beijing Aerospace Propulsion Institute | 1.00 | infobox |
| YF-73 | Diameter | 2.2 metres (7 ft 3 in) | 1.00 | infobox |
| YF-73 | Dry mass | 236 kilograms (520 lb) | 1.00 | infobox |
| YF-73 | First flight | 1984-01-29 | 1.00 | infobox |
| YF-73 | Last flight | 2000-05-26 | 1.00 | infobox |
| YF-73 | Length | 1.44 metres (4 ft 9 in) | 1.00 | infobox |
| YF-73 | Manufacturer | China Academy of Launch Vehicle Technology (CALT) | 1.00 | infobox |
| YF-73 | Mixture ratio | 5.00 | 1.00 | infobox |
| YF-73 | Nozzle ratio | 40 | 1.00 | infobox |
| YF-73 | Propellant | Liquid oxygen / Liquid hydrogen | 1.00 | infobox |
| YF-73 | Specific impulse, vacuum | 420 seconds (4.1 km/s) | 1.00 | infobox |
| YF-73 | Status | Retired | 1.00 | infobox |
| YF-73 | Successor | YF-75 | 1.00 | infobox |
| YF-73 | Thrust, vacuum | 44.15 kilonewtons (9,930 lbf) | 1.00 | infobox |
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