Jakovlev / Jakowlew / Yakovlev Jak-23 / Yak-23
Photo ©: Anton Balakchiev (Photos at airliners.net)
Jak-23 / Yak-23
Fighter
| Crew | 1 | |
| Propulsion | 1 Turbojet Engine | |
| Engine Model | Klimow / Klimov RD-500 | |
| Engine Power | 15,6 kN | 3507 lbf |
| Speed | 922 km/h | 498 kts 573 mph |
| Service Ceiling | 14.000 m | 45.932 ft |
| Range | 500 km | 270 NM 311 mi. |
| Empty Weight | 2.200 kg | 4.850 lbs |
| max. Takeoff Weight | 3.300 kg | 7.275 lbs |
| Wing Span | 8,73 m | 28,6 ft |
| Wing Area | 13,5 m² | 145 ft² |
| Length | 8,33 m | 27,3 ft |
| Height | 3,30 m | 10,8 ft |
| First Flight | 08. Jul. 1947 | |
| Production Status | out of production | |
| Production Range | 1949-1951 | |
| Total Production | 310 | |
| Developed from | Jakowlew Jak-15 & Jak-17 / Yakovlev Yak-15 & Yak-17 | |
| NATO Code | Flora | |
| Data for (Version) | Yakovlev Yak-23UTI / Jakowlew Jak-23UTI | |
| Weblinks | Extras |
| A.S.Yakovlev Design Bureau |
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