Single-place fighter equipped with radar. MiG-19PM version has only missile armament, unlike basic version MiG-19.
MiG-19 was first supersonic fighter serially produced and put into service. Aircraft was developed at a base of SM-2 test aircraft. Prototype SM-9 (improved SM-2) was equipped with two engine Tumanskij AM-9B has maiden flight at 5th of January 1954 piloted by G. A. Sedov. Even before end of tests SM-19 under designation MiG-19 entered into production and from 1954 it was put into service. More than 2000 aircraft of all versions was made in USSR. Under designation S.105 was MiG-19S produced under licence in Czechoslovakia. There were built 103 aircrafts. MiG-19S was made in China under licence under designation J-6. J-6 I and J-6 II were in China under licence built MiG-19P and MiG-19PM.
Aircraft MiG-19PM was equipped with radar Izumrud-2 (Emerald) RP-1U, later series with RP-2U. Radar has range of 12 km and guiding range from 6 to 8 km. Aircraft with radar is 360 mm longer than version MiG-19S.
Armament consist of four missiles RS-1U in early versions, later of RS-2U missiles (NATO code AA-1 Alkali).
Czechoslovakia obtained 33 MiG-19PM from 1959 to 1960. One of them with number 1113 became an exhibit of the Museum.
								Specification of MiG-19PM: | 
						|
| wing span: | 9,00 m | 
| length: | 13,25 m | 
| height: | 3,90 m | 
| wing area: | 25,00 m2 | 
| weight: | |
| - empty aircraft | 5673 kg | 
| - normal take-off | 7730 kg | 
| - take-off with two 400l external fuel tanks | 8464 kg | 
| internal fuel: | 1800 kg | 
| engine: | 2 x Tumanskij AM-9B (RD-9B) | 
| maximal thrust: | 2 x 31,88 kN | 
| maximal speed: | |
| - in altitude 10000 m | 1250 km/h (Mach = 1,15) | 
| - in altitude 15000 m | 1130 km/h (Mach = 1,06) | 
| range in altitude 10000m: | 1000 km without external tanks | 
| climbing to 15000m: | 4,8 min | 
| service ceiling: | 17250 m | 
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© Kamil Pankuch 2004-2007
					airmuseum.kosice at gmail.com