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==Background==
==Background==
Prior to the 1995 Crisis in Sulania, an overwhelming amount of the aviation proportion of the Kalaronian MIC was directed towards the production of Light Fighters, such as the K-10 and K-12, that were designed around the concept of providing cheap and affordable comb
Although experiences in the Flynnvakian-Baxtonian War had shown Kalaronian Military Analysists that the Light Fighter as a concept was becoming less capable against more heavily armed, faster, and better equipped aircraft; there was relatively little interest in the ITF-aligned nations for the more expensive airframes required, or for the heavier development fees. Meanwhile, the USCS (the primary counterpart to the ITF) maintained consistent orders for the treaty-protected K.17, a larger Strike Fighter designed around a heavy airframe and the powerful QWS-110 Engines, since the start of the decade.
 
This restriction was harmlessly ignored for years, as the lack of international interest in the concept, as well as then peaceful relations with the USCS, disincentivized the production of a wholly separate Aircraft. However
==Development==
==Development==



Revision as of 06:06, 23 February 2021

K-26
K26-ACE.png
An airborne K-26A
General information
TypeFighter
StatusActive
History
Manufactured1996-Present
Introduction date1998

Background

Although experiences in the Flynnvakian-Baxtonian War had shown Kalaronian Military Analysists that the Light Fighter as a concept was becoming less capable against more heavily armed, faster, and better equipped aircraft; there was relatively little interest in the ITF-aligned nations for the more expensive airframes required, or for the heavier development fees. Meanwhile, the USCS (the primary counterpart to the ITF) maintained consistent orders for the treaty-protected K.17, a larger Strike Fighter designed around a heavy airframe and the powerful QWS-110 Engines, since the start of the decade.

This restriction was harmlessly ignored for years, as the lack of international interest in the concept, as well as then peaceful relations with the USCS, disincentivized the production of a wholly separate Aircraft. However

Development

Design

Operational history

Early service

Anti-bomber operations

Post-war service

Variants

The prototype flown in the 1939 fighter competition was designated Chikai WH 25, with WH indicating wŏnhyŏng (prototype). Six were built. Its armament consisted of four 7.5mm machine guns: two above the nose, and one in each wing. Each gun was fed from a 500-round belt.

Type 40-I

Type 40-II

Type 40-III

Type 40-IV

Type 40-V

Specifications (Type 40-I)

General Characteristics

  • Crew:
  • Length:
  • Wingspan:
  • Height:
  • Wing Area:
  • Empty Weight:
  • Loaded Weight:
  • Powerplant:

Performance

  • Maximum Speed:
  • Range:
  • Service Ceiling:
  • Rate of Climb:
  • Wing Loading:
  • Power-to-Mass ratio:

Armament

  • Guns:
    2x forward-firing
    2x forward-firing
  • Bombs:

See also