TupolevANT-23 I-12ANT-23bis |
![]() Tupolev I-12 |
The experimental Tupolev ANT-23 was designed around two large-caliber recoilless guns, integrated into tandem tailbooms. The aircraft was fitted with two radial engines in a push-pull configuration, and received the official designation of I-12. Even with twin engines, the aircraft was underpowered, as the rear engine was inefficient, and the design suffered from higher-than-expected drag, due in part to the externally reinforced wings and tail. The rear-mounted propellor also presented difficulties should in-flight pilot egress be necessitated. During an inflight gun test, a round exploded in the port gun, causing damage to the tailboom on landing. An improved prototype, the ANT-23bis, with jettisonable rear propellor, was under construction when the program was cancelled.

Timeline
| Specifications | I-12 |
| Designer(s) | Viktor Nikolayevich Chernyshyov |
| Mission Type | Experimental fighter prototype |
| Powerplant | 2 x 525 hp GR9AK (license-built Gnome-Rhône 9AK) 9 cyl. radials |
| Dimensions | |
| Span | 51 ft 5 in (15.67 m) |
| Length | 31 ft 2.75 in (9.52 m) |
| Height | ? |
| Wing area | 322.93 - 355.00 sq ft (30.00 - 33.00 m2) |
| Weights | |
| Empty | 4,008 lb (1,818 kg) |
| Loaded | 5,302 lb (2,405 kg) |
| Max | ? |
| Performance | |
| Max speed | 186 mp @ sl (300 km/hr) 174 - 198 mph @ 16,405 ft (280 - 318 km/hr @ 5,000 m) |
| Cruise speed | -- |
| Time to 16,405 ft (5,000 m) | 7.7 min |
| Service ceiling | 30,580 ft (9,320 m) |
| Range | 252 miles (405 km) |
| Armament | 2 x 76 mm Kurchevski APK-4 recoilless guns in tailbooms |
| Crew | One |
| User | USSR (not operational) |
| Number built | One ANT-23, plus one partially built ANT-23bis |
| Construction Numbers | ? |
| Serial Numbers | ? |
| Test Pilots | I. F. Kozlov |
| Unofficial Nickname | Baumanskii Komsomolyets |
Web Links
Sources
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© 1997-2005, Robert Beechy
http://fire.prohosting.com/hud607/uncommon/aircraft/i-12/index.html
Originally posted January 2005
Modified: 01/01/2005