Daesŭngri DS-1: Difference between revisions
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* {{flag|Dzhungestan}}: 56 units sold to Communist forces in 1974 | * {{flag|Dzhungestan}}: 56 units sold to Communist forces in 1974 | ||
* {{flagicon|Menghe|1964}} [[Democratic People's Republic of Menghe]] | * {{flagicon|Menghe|1964}} [[Democratic People's Republic of Menghe]] | ||
==Specifications (DS-1G)== | |||
{{aircraft specifications | |||
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]]. --> | |||
| plane or copter? = plane | |||
| jet or prop? = jet | |||
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item does not apply, like capacity, leave it blank. | |||
--> | |||
| ref = | |||
<!-- General characteristics --> | |||
| crew = 1 | |||
| capacity = | |||
| payload main = | |||
| payload alt = | |||
| payload more = | |||
| length main = 11.26 m | |||
| length alt = 37 ft | |||
| span main = 9.63 m | |||
| span alt = 31 ft 7 in | |||
| height main = 3.8 m | |||
| height alt = 12 ft 6 in | |||
| area main = 22.6 m<sup>2</sup> | |||
| area alt = 243.3 ft<sup>2</sup> | |||
| airfoil = | |||
| aspect ratio = | |||
| empty weight main = 3,870 kg | |||
| empty weight alt = 8,532 lb | |||
| useful load main = | |||
| useful load alt = | |||
| loaded weight main = 5,290 kg | |||
| loaded weight alt = 11,660 lb | |||
| max takeoff weight main = 6,050 kg | |||
| max takeoff weight alt = 13,340 lb | |||
| more general = | |||
<!-- Powerplant, jet engine(s) --> | |||
| engine (jet) = {{wp|Klimov VK-1}}F | |||
| type of jet = {{wp|afterburner|afterurning}} {{wp|turbojet}} | |||
| number of jets = 1 | |||
| thrust main = 26.5 kN | |||
| thrust alt = 5,955 lbf | |||
| thrust original = | |||
| afterburning thrust main = 33.8 kN | |||
| afterburning thrust alt = 7,423 lbf | |||
<!-- Powerplant, prop(s) --> | |||
| engine (prop) = | |||
| type of prop = | |||
| number of props = | |||
| power main = | |||
| power alt = | |||
| power original = | |||
<!-- Powerplant, propellor/rotor details --> | |||
| propeller or rotor? = <!-- options: propeller/rotor --> | |||
| propellers = | |||
| number of propellers per engine = | |||
| propeller diameter main = | |||
| propeller diameter alt = | |||
| more general powerplant = | |||
<!-- Performance --> | |||
| max speed main = 1,150 km/h | |||
| max speed alt = Mach 0.93 | |||
| max speed more = | |||
| cruise speed main = | |||
| cruise speed alt = | |||
| cruise speed more = | |||
| stall speed main = | |||
| stall speed alt = | |||
| stall speed more = | |||
| never exceed speed main = | |||
| never exceed speed alt = | |||
| range main = | |||
| range alt = | |||
| range more = | |||
| combat radius main= | |||
| combat radius alt = | |||
| combat radius more= | |||
| ferry range main = 2,020 km | |||
| ferry range alt = 1,255 mi | |||
| ferry range more = at 12,000 m with 2x 400L drop tanks | |||
| endurance = | |||
| ceiling main = 16,600 m | |||
| ceiling alt = 54,450 ft | |||
| ceiling more = with afterburner | |||
| climb rate main = 65 m/s | |||
| climb rate alt = 12,800 ft/min | |||
| climb rate more = | |||
| sink rate main = | |||
| sink rate alt = | |||
| sink rate more = | |||
| loading main = 268.4 kg/m<sup>2</sup> | |||
| loading alt = 55 lb/ft<sup>2</sup> | |||
| thrust/weight = 0.63 | |||
| power/mass main = | |||
| power/mass alt = | |||
| more performance = | |||
<!-- Armament --> | |||
| guns = * 2 × 23mm autocannon (80 rounds per gun)<br> | |||
* 1 × 37mm autocannon (40 rounds total) | |||
| bombs = | |||
| rockets = | |||
| missiles = | |||
| hardpoints = 2 hardpoints | |||
| hardpoint capacity = 500 kg | |||
| hardpoint rockets = 2 × UB-16-57 rocket pods for {{wp|S-5 rocket}}s | |||
| hardpoint missiles = | |||
| hardpoint bombs = 2 × 250 kg (550 lb) bombs | |||
| hardpoint other = 2 × 400L drop tank | |||
| avionics = | |||
}} | |||
[[Category:Menghe]] | [[Category:Menghe]] |
Latest revision as of 19:48, 10 April 2019
Daesŭngri DS-1 | |
---|---|
DS-1G in the Dongchŏn Military Museum | |
Role | Fighter aircraft |
National origin | DPRM |
Manufacturer | Daesŭngri Aviation Bureau |
Introduction | 1965 |
Primary users | Menghean People's Army (historical) Dzhungestani Air Force (historical) |
Produced | 1965-1970 |
Number built | 451 |
Developed from | Mikoyan-Gurevich MiG-17 |
The Daesŭngri DS-1 (Formal designation: 대승리 1호 전투기 / 大勝利一號戰鬪機, Daesŭngri Il-ho Jŏntugi, "Daesŭngri No.1 Fighter;" Short designation 대승리-1 Daesŭngri-il "Daesŭngri-1") is a Menghean-built version of the Letnian Mikoyan-Gurevich MiG-17 single-seat jet fighter. For a few years after its introduction it was also designated Type 65, with the designation DS-1 first appearing around 1970. Already obsolete at the time of its introduction, it is no longer in active service with the Menghean armed forces.
History
Menghean pilots gained extensive experience flying the MiG-17 during the late stages of the Menghean War of Liberation, using airframes which were sold to Polvokia and later smuggled across the northern border. Despite its lack of missiles and supersonic capability, the MiG-17 made a favorable impression on Menghean pilots.
As the war neared its end, Menghe secured a license from Letnia to produce the MiG-17 domestically. Plans were delivered in 1964, and factory equipment was delivered in the same year, accompanied by knockdown kits for asembling the first 34 airframes. The Daesŭngri Aircraft Production Bureau set up an assembly center in a factory complex in Girim province, which the Menghean Liberation Army had already been using as a MiG-17 repair site since 1962, and production began in the summer of 1965.
Design
The baseline Type 65G (DS-1G) is essentially identical to the MiG-17AS, the multirole variant of the MiG-17 with limited ground-attack capability. It has two under-wing hardpoints, which can be used to carry 250-kg unguided bombs or UB-16-57 rocket pods. It lacks any kind of radar, even a ranging set, and also lacks the ability to carry heat-seeking air-to-air missiles. In air-to-air combat, it is entirely reliant on its gun armament.
A two-seat trainer variant was also produced. Somewhat confusingly, it was originally designated Type 65N, but later changed to DS-1G2. Originally it was intended as a lead-in trainer for the DS-1G, with two DS-1G2s per 18-plane squadron. After the DS-1G was deemed obsolete and the DS-2 emerged as its replacement, production of the DS-1 switched over to the DS-1G2 variant, which accounted for all production in 1969 and 1970. These airframes were used as trainers for the DS-2, which lacked a lead-in trainer variant until the introduction of the DS-2N2 in 1970.
By the late 1970s, the DS-1 was widely regarded as obsolete, and the Menghean People's Air Force began to retire it from front-line service. Many DS-1G airframes were converted to radio-controlled drones, designated DS-1PJG (Pyojŏkgi, "target plane") and used for air-to-air and surface-to-air missile testing. Large numbers of DS-1G2s remained in use as intermediate trainers between propeller planes and service jets like the DS-5 and SR-6, but there are some reports of DS-1G2s being converted to target drones, in which case they bore the same DS-1PJG designation.
Variants
- DS-1G: Single-seater fighter variant, originally known as Type 65G. 213 produced.
- DS-1G2: Twin-seater lead-in trainer, originally known as Type 65N. 225 produced, most after 1967.
- DS-1RD: Possible designation for a prototype with a ranging radar in the middle of the nose splitter, likely a copy of the "Izmrud" radar from the MiG-17P. 1 built.
- DS-1JPG: Prototype fighter-bomber with modified hardpoints for heavier bombs. 2 built. Rejected in favor of the DS-2.
- DS-1PJG: Unmanned target drone made from converted DS-1 airframes.
Operators
- Dzhungestan: 56 units sold to Communist forces in 1974
- Democratic People's Republic of Menghe
Specifications (DS-1G)
General characteristics
- Crew: 1
- Length: 11.26 m (37 ft)
- Wingspan: 9.63 m (31 ft 7 in)
- Height: 3.8 m (12 ft 6 in)
- Wing area: 22.6 m2 (243.3 ft2)
- Empty weight: 3,870 kg (8,532 lb)
- Loaded weight: 5,290 kg (11,660 lb)
- Max. takeoff weight: 6,050 kg (13,340 lb)
- Powerplant: 1 × Klimov VK-1F afterurning turbojet
- Dry thrust: 26.5 kN (5,955 lbf)
- Thrust with afterburner: 33.8 kN (7,423 lbf)
Performance
- Maximum speed: 1,150 km/h (Mach 0.93)
- Ferry range: 2,020 km (1,255 mi) at 12,000 m with 2x 400L drop tanks
- Service ceiling: 16,600 m (54,450 ft) with afterburner
- Rate of climb: 65 m/s (12,800 ft/min)
- Wing loading: 268.4 kg/m2 (55 lb/ft2)
- Thrust/weight: 0.63
Armament
- Guns:
- 2 × 23mm autocannon (80 rounds per gun)
- 1 × 37mm autocannon (40 rounds total)
- Hardpoints: 2 hardpoints with a capacity of 500 kg and provisions to carry combinations of:
- Rockets: 2 × UB-16-57 rocket pods for S-5 rockets
- Bombs: 2 × 250 kg (550 lb) bombs
- Other: 2 × 400L drop tank