The Yakovlev Yak-23 was the final iteration of the post-war turbojet designs beginning with the Yak-15 and continuing in the Yak-17 aircraft series. The Yak-23 was similar to the Yak-17 but differed in the utilization of higher-mounted horizontal tail surfacing. Another key difference in the design lay in the larger tail rudder design assembly.
The Yak-23 was a single-engine, single-crew jet-powered aircraft designed on a rudimentary fuselage. A straight-winged design - popular with jet designs of the time - adorned either site of the mid-to-rear mounted cockpit. The cockpit area sunk into the rearward part of the fuselage, adding to the aerodynamic element. The front of the fuselage was dominated by a cone-less intake opening with the turbojet exhaust located at mid-fuselage, just under the pilots seating arrangement. A powered tricycle-type landing gear rounded out the key technological engineering features.
Termed a "light-weight day fighter", the Yak-23 was armed with two 23mm cannons mounted in the nose - this being the now popular alternative to the machine gun-laced fighter designs of the Second World War. A single 132lb conventional bomb could be carrier under-fuselage as well, adding a hint of multirole capabilities.
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.
Specifications
Yakovlev - USSR Manufacturer(s)
Bulgaria; Czechoslovakia; Poland; Romania; Soviet Union Operators
AIR-TO-AIR COMBAT
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
26.6 ft (8.12 meters) Length
28.6 ft (8.73 meters) Width/Span
10.9 ft (3.31 meters) Height
4,409 lb (2,000 kilograms) Empty Weight
6,693 lb (3,036 kilograms) Maximum Take-Off Weight
+2,284 lb (+1,036 kg) Weight Difference
1 x Klimov RD-500 turbojet engine developing 3,505 lb of thrust. Propulsion
The "Military Factory" name and MilitaryFactory.com logo are registered ® U.S. trademarks protected by all applicable domestic and international intellectual property laws. All written content, illustrations, and photography are unique to this website (unless where indicated) and not for reuse/reproduction in any form. Material presented throughout this website is for historical and entertainment value only and should not to be construed as usable for hardware restoration, maintenance, or general operation. We do not sell any of the items showcased on this site. Please direct all other inquiries to militaryfactory AT gmail.com. No A.I. was used in the generation of this content; site is 100% curated by humans.