The DF-113 is a supersonic jet fighter that China planned to develop during the Great Leap Forward in the late 1950s. Designed by Harbin Military Engineering Institute. In the spring of 1958, some teachers and students of the Air Force Engineering Department of Kazakhstan Military Industry proposed the design of a new fighter aircraft, which would fight against the F-105 and B-58 of the United States. However, it was too radical a design for China's capabilities at the time, so the project was eventually abandoned.The data used in this work are those measured by a small scale model at that time. Wheel heading will be locked after the speed rich at about 70km/h. AG1:afterburner; AG2: Weapon system: AG3
Specifications
General Characteristics
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- Wingspan 33.9ft (10.3m)
- Length 72.4ft (22.1m)
- Height 18.4ft (5.6m)
- Empty Weight N/A
- Loaded Weight 23,355lbs (10,593kg)
Performance
- Power/Weight Ratio 10.969
- Wing Loading 29.3lbs/ft2 (143.3kg/m2)
- Wing Area 795.9ft2 (73.9m2)
- Drag Points 8565
Parts
- Number of Parts 692
- Control Surfaces 7
- Performance Cost 3,213
【夭折战机复刻计划】
东风-113，是20世纪50年代末中国在大跃进时期计划研制的超音速喷气式歼击机。由哈尔滨军事工程学院设计。在1958年春，哈军工空军工程系部分师生提出设计新式战斗机的要求，其作战对象为美国的F-105和B-58。但它严重抛离了科技发展与工业基础，设计过于激进，超出当时中国的能力范围，于是项目最终下马。本作所用数据为当时通过小比例模型测得的数据。机轮带有超速航向自锁功能。AG1：加力；AG2：武器系统：AG3：GPWS；AG4：座舱盖；AG5：滑行灯；AG6：减速伞（8秒后自抛离）；AG7：弹射；AG8：电子设施；VTOL：襟翼
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