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^{[citation needed]}
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.^[1] 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

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GSh-30-2
GSh-30-2K

Specifications (GSh-30-2)

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Manufacturer: KBP Instrument Design Bureau
Type: dual-barrel autocannon
Caliber: 30×165 mm, 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^{[citation needed]}
Muzzle velocity: 870 m/s
Projectile weight: 390 g
Mounting platforms: Sukhoi Su-25 "Frogfoot"

Specifications (GSh-30-2K)

[edit]

Manufacturer: KBP Instrument Design Bureau
Type: dual-barrel autocannon
Caliber: 30×165 mm
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”

Users

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References

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^ "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

[edit]

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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Wikimedia Commons has media related to GSh-30.

Russian and former Soviet aircraft ordnance

Missiles

Air-to-air	K-5 R-3 R-8 R-38 R-4 R-40 R-23 R-60 R-33 R-27 R-73 R-77 R-37
Air-to-surface	Kh-23 Kh-25 Kh-28 Kh-29 Kh-45 Kh-58 Kh-59 LMUR
Anti-ship, cruise	KS-1 K-10S Kh-20 Kh-22 KSR-2 KSR-5 Kh-55 Kh-15 Kh-31 Kh-35 Kh-45 Kh-90
Anti-tank	3M6 Shmel 9M17 Fleyta 9M14 Malyutka 9K114 Shturm 9M120 Ataka 9K121 Vikhr

Rockets

Aerial bombs

Autocannons,
machine guns

7.62 mm	SIBEMAS PV-1 DA ShKAS Savin–Norov GShG-7.62
12.7 mm	ShVAK 12.7 mm Berezin UB Afanasev A-12.7 YakB-12.7
20 mm	Sh-3 ShVAK 20 mm Berezin B-20
23 mm	VYa-23 NS-23 NR-23 AM-23 R-23 GSh-23 GSh-6-23
30 mm	NR-30 GSh-30-1 GSh-30-2 GSh-6-30 2A42
37 mm	Sh-37 NS-37 N-37
45 mm	NS-45
57 mm	N-57/OKB-16-57 RShR-57/OKB-15-57

Variants

Specifications (GSh-30-2)

Specifications (GSh-30-2K)

See also

Users

References

Sources

External links