| In the late 'sixties, a team under the leadership of Lu
Xiao-Pcheng initiated design of a lightweight single-seat
air superiority fighter at the NAMC (Nanchang Aircraft
Manufacturing Company) under the designation
J-12 (Jianjiji-12). Powered by a single WP-6 (Chinese-built Tumansky RD-9BF-811) with a maximum rating of
3454kg, the first of three prototypes was
flown on 26 December 1970. Owing to the indifferent results
achieved during flight testing, the J-12 was subjected
to considerable redesign. The structure was simplified
and lightened, area ruling was applied to the
fuselage, the air intake was redesigned, the gun armament
was moved aft and simple split flaps supplanted
an arrangement of slats and triple-slotted flaps. The extensively
revised J-12 flew as a prototype in July 1975,
and six pre-series aircraft were built, these each carrying
an armament of one 23mm and one 30mm cannon.
A total of 61 hrs 12 min of flight testing had been accumulated
in 135 test flights by January 1977, when further
development was discontinued owing to the superior
characteristics of the J-7 (licence-built MiG-21F-13)
already with the People's Republic of China Air Force.
| A three-view drawing (1663 x 1240) |
WEIGHTS |
Take-off weight | 4530 kg | 9987 lb |
Empty weight | 3172 kg | 6993 lb |
DIMENSIONS |
Wingspan | 7.20 m | 24 ft 7 in |
Length | 10.30 m | 34 ft 10 in |
Height | 3.73 m | 12 ft 3 in |
PERFORMANCE |
Max. speed | 1300 km/h | 808 mph |
Ceiling | 16970 m | 55700 ft |
Range | 688 km | 428 miles |
paidui, 18.06.2011 10:59 (licence-built MiG-21F-13) already with the People's Republic of China Air Force. reply |
Chinese, 29.01.2011 16:02 Its arm was 2*23mm cannons reply |
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