Akula TK-22: Difference between revisions

Jump to navigation Jump to search
Line 78: Line 78:
|eng1 kn=<!-- jet/rocket engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 note={{cvt|1277|PS|kW hp|0}}
|eng1 note={{cvt|1724|PS|kW hp|0}}


|prop blade number=3
|prop blade number=3

Revision as of 05:24, 29 January 2022

Akula TK-22
Akula TK-22 formation over the Khastravali Mountains.jpg
Early production TK-22s in formation over the Southern Khastravali Mountains
Role Medium bomber
National origin Tennai
Manufacturer Akula Aircraft Company
Designer Vadiaya Sera Bamraulia
First flight May 1934
Introduction March 1935
Retired 1950
Status Retired
Primary user Royal Tennaiite Air Force
Produced 1935-1945
Number built 6,389

The Akula TK-22 was a Tennaiite medium bomber during the Siduri War. It began operation in 1936 where it was used extensively in tactical bombing missions and also in attacking enemy shipping. It was used in operations all across the Tennaiite Front, into Shirvaniya, ships and ports in the seas of Western Siduri, and Syara in the later stages of the war. It along with the Parvati PTK-23 served as the primary medium bombers of the Siduri War.

Design and Development

Operational history

Siduri War

Variants

TK-22
Original production model. 118 were produced before production switched to the 22-IB
TK-22-IB
Clear upper cabin replaced with rotating turret and more powerful Curavali AC112 engines (1,700 hp). Five additional 12.7 mm machine guns added.
TK-22-IC
Tk-22-II
Tk-22-IIB

Operators

Specifications (TK-22-IB)

General characteristics

  • Crew: six
  • Length: 19.2 m (63 ft 0 in)
  • Wingspan: 27 m (88 ft 7 in)
  • Height: 5.32 m (17 ft 5 in)
  • Wing area: 83 m2 (890 sq ft)
  • Empty weight: 8,917 kg (19,659 lb)
  • Max takeoff weight: 15,876 kg (35,001 lb)
  • Powerplant: 2 × Akula Curavali AC44 14-cylinder air-cooled radial piston engine 1,724 PS (1,268 kW; 1,700 hp)
  • Propellers: 3-bladed variable-pitch propellers

Performance

  • Maximum speed: 431 km/h (268 mph; 233 kn)
  • Cruise speed: 345 km/h (214 mph; 186 kn)
  • Range: 2,600 km (1,616 mi; 1,404 nmi)
  • Service ceiling: 10,000 m (33,000 ft)
  • Time to altitude: 6,000 m (19,685 ft) in 13 minutes 48 seconds

Armament

  • Guns:
  • 7× 12.7 mm (.50 in) machine guns
  • Bombs:
  • 2,000 kg (4,500 lb) lb of bombs