| Gryazev-Shipunov GSh-30-2 | |
|---|---|
 GSh-30-2 on a Sukhoi Su-25 | |
| Type | Dual-barrel aircraft autocannon |
| Service history | |
| In service | 1981–present |
| Production history | |
| Designer | KBP |
| Manufacturer | KBP |
| Specifications | |
| Mass | GSh-30-2: 105 kilograms (231 lb) GSh-30-2k: 126 kilograms (278 lb) |
| Length | GSh-30-2: 2,044 millimetres (6.706 ft) GSh-30-2k: 2,944 millimetres (9.659 ft) |
| Barrel length | GSh-30-2: 1,500 millimetres (4.9 ft) GSh-30-2k: 2,400 millimetres (7.9 ft) |
| Shell | 30×165mm |
| Caliber | 30mm |
| Barrels | 2 |
| Action | Gast principle |
| Rate of fire | 1,000-3,000 rpm |
| Muzzle velocity | 870 m/s (2,850 ft/s) |
| Maximum firing range | ~1,800m |
The Gryazev-Shipunov GSh-30-2 (ГШ-30-2) or GSh-2-30 is a Soviet dual-barrel autocannon developed for use on certain ground attack military aircraft and helicopters.
The cannon is not related to the Gryazev-Shipunov GSh-30-1, but is a recoil-operated cannon using the Gast principle, like the Gryazev-Shipunov GSh-23L.
The GSh-30-2 was designed for the Sukhoi Su-25 ground attack plane, it can also be carried in external gun pods and mounted on the Pakistani-Chinese JF-17 Thunder. It measures 2,044 × 222 × 195 mm, with a barrel length of 1500 mm and a weight of 105 kg. The GSh-30K is a modified version with 2400 mm long water-cooled barrels, a variable rate of fire, and dimensions of 2,944 × 222 × 195 mm. It is used on a fixed mounting on late model Mil Mi-24 helicopters, e.g. the Mi-24P.
Variants
- GSh-30-2
- GSh-30-2K
Specifications (GSh-30-2)
- Manufacturer: KBP Instrument Design Bureau
- Type: dual-barrel autocannon
- Caliber: 30×165mm, electrically primed
- Operation: recoil operation
- Length: 2,044 mm
- Barrel Length: 1,500 mm
- Weight (complete): 105 kg
- Rate of fire: 1,000–3,000 rpm
- Muzzle velocity: 870 m/s
- Projectile weight: 390 g
- Mounting platforms: Sukhoi Su-25 "Frogfoot"
Specifications (GSh-30-2K)
- Manufacturer: KBP Instrument Design Bureau
- Type: dual-barrel autocannon
- Caliber: 30×165mm
- Operation: recoil operation
- Length: 2,944 mm
- Barrel Length: 2,400 mm
- Weight (complete): 126 kg
- Rate of fire: 300 rpm (low) – 2,000–2,600 rpm (high)
- Muzzle velocity: 940 m/s
- Projectile weight: 390 g
- Mounting platforms: Mil Mi-24P "Hind", Sukhoi Su-25 “Frogfoot”
See also
Users
References
- "FC-1 (JF-17 Thunder) Multirole Fighter Aircraft - SinoDefence.com". 2013-04-02. Archived from the original on 2013-04-02. Retrieved 2023-02-09.
Sources
 | This article includes a list of references, related reading, or external links, but its sources remain unclear because it lacks inline citations. Please help improve this article by introducing more precise citations. (November 2014) (Learn how and when to remove this message) |
- Koll, Christian (2009). Soviet Cannon: A Comprehensive Study of Soviet Arms and Ammunition in Calibres 12.7mm to 57mm. Austria: Koll. p. 303. ISBN 978-3-200-01445-9.
- "KBP Instrument Design Bureau - Corporative Site". 17 July 2013. Archived from the original on 2013-07-17.
External links
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