HH2 Attack Helicopter: Difference between revisions
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|introduction = 14 May 1992 | |introduction = 14 May 1992 | ||
|retired = | |retired = | ||
|status = In service | |status = In active service | ||
|primary user = [[Ruvelkan Imperial Air Force]] | |primary user = [[Image:RIAFFlag.png|border|22px]] [[Ruvelkan Imperial Air Force]] | ||
|more users = | |more users = | ||
|produced = 1990 – Present | |produced = 1990 – Present | ||
|number built = ~ | |number built = ~550 | ||
|unit cost = | |unit cost = | ||
|developed from = Kormos V-80 | |developed from = Kormos V-80 | ||
| Line 40: | Line 40: | ||
==Specifications== | ==Specifications== | ||
[[File:Kamov Ka-50 Hokum graphic.gif|thumb|350px|Kormos HH2 line drawing.]] | |||
===General Characteristics=== | |||
* '''Crew:''' 1 | |||
* '''Length:''' 16 m (52 ft 6 in) | |||
* '''Height:''' 4.93 m (16 ft 2 in) | |||
* '''Empty Weight:''' 7,700 kg (16,976 lbs) | |||
* '''Gross Weight:''' 9,800 kg (21,605 lbs) | |||
* '''Max Takeoff Weight:''' 10,800 kg (23,810 lbs) | |||
* '''Powerplant:''' 2 × Kormos K2500 turboshaft engines, 1,800 kW (2,400 shp) each | |||
* '''Main Rotor Diameter:''' 2 × 14.5 m (47 ft 7 in) | |||
* '''Main Rotor Area:''' 330.3 m² (3,555 sq ft) contra-rotating 3-bladed main rotors | |||
===Performance=== | |||
* '''Maximum Speed:''' 315 km/h (196 mph; 170 kn) | |||
* '''Cruise Speed:''' 270 km/h (168 mph; 146 kn) | |||
* '''Never Exceed Speed:''' 350 km/h (217 mph; 189 kn) | |||
* '''Range:''' 545 km (339 mi; 294 nmi) | |||
* '''Combat Range:''' 470 km (292 mi; 254 nmi) | |||
* '''Service Ceiling:''' 5,500 m (18,000 ft) | |||
* '''Rate of Climb:''' 12 m/s (2,400 ft/min) | |||
* '''Disk Loading:''' 30 kg/m² (6.1 lb/ft²) | |||
* '''Power/Mass:''' 0.3 kW/kg (0.20 hp/lb) | |||
===Armament=== | |||
* '''Guns:''' 1 × 30 mm cannon with 460 rounds | |||
* '''Hardpoints:''' 6 hardpoints (4 underwing, 2 wingtip); 2 wingtip pods armed with chaff and flare countermeasures. | |||
[[Category:Ruvelka]] | [[Category:Ruvelka]] | ||
[[Category:Military of Ruvelka]] | |||
[[Category:Ruvelkan Helicopters]] | |||
Latest revision as of 05:45, 12 August 2020
 | This article is incomplete because it is pending further input from participants, or it is a work-in-progress by one author. Please comment on this article's talk page to share your input, comments and questions. Note: To contribute to this article, you may need to seek help from the author(s) of this page. |
| HH2 Sólyom | |
|---|---|
| |
| A Kormos HH2 of the Ruvelkan Imperial Air Force. | |
| Role | Attack helicopter, scout helicopter |
| National origin |  Ruvelka
|
| Manufacturer | Kormos |
| First flight | 23 June 1988 |
| Introduction | 14 May 1992 |
| Status | In active service |
| Primary user |  Ruvelkan Imperial Air Force
|
| Produced | 1990 – Present |
| Number built | ~550 |
| Developed from | Kormos V-80 |
The Kormos HH2 Sólyom is a single-seat Ruvelkan all-weather, day-night, attack helicopter utilizing a coaxial rotor system. Designed in the 1980s, the Sólyom was adopted by the Ruvelkan Imperial Air Force in 1992 as a dedicated attack helicopter to support the larger and less-maneuverable HH1 gunships. The Sólyom served extensively during the Zemplen War with the RIAF's Special Air Service. It was the primary tool Ruvelka utilized for night-raiding Syaran armor and supply trains, earning it the nickname Phantom by Syaran forces.
Development
Design
Operational History
Imerti Conflict
Zemplen War
Specifications
General Characteristics
- Crew: 1
- Length: 16 m (52 ft 6 in)
- Height: 4.93 m (16 ft 2 in)
- Empty Weight: 7,700 kg (16,976 lbs)
- Gross Weight: 9,800 kg (21,605 lbs)
- Max Takeoff Weight: 10,800 kg (23,810 lbs)
- Powerplant: 2 × Kormos K2500 turboshaft engines, 1,800 kW (2,400 shp) each
- Main Rotor Diameter: 2 × 14.5 m (47 ft 7 in)
- Main Rotor Area: 330.3 m² (3,555 sq ft) contra-rotating 3-bladed main rotors
Performance
- Maximum Speed: 315 km/h (196 mph; 170 kn)
- Cruise Speed: 270 km/h (168 mph; 146 kn)
- Never Exceed Speed: 350 km/h (217 mph; 189 kn)
- Range: 545 km (339 mi; 294 nmi)
- Combat Range: 470 km (292 mi; 254 nmi)
- Service Ceiling: 5,500 m (18,000 ft)
- Rate of Climb: 12 m/s (2,400 ft/min)
- Disk Loading: 30 kg/m² (6.1 lb/ft²)
- Power/Mass: 0.3 kW/kg (0.20 hp/lb)
Armament
- Guns: 1 × 30 mm cannon with 460 rounds
- Hardpoints: 6 hardpoints (4 underwing, 2 wingtip); 2 wingtip pods armed with chaff and flare countermeasures.