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И—360(图纸代号CM—2)是超音速前线歼击机的原型机。它是在综合了И—340的发动机试验成果和И—350的大后掠机翼试验成果的基础上研制的。首架原型机CM—2/1(图一)于1952年5月24日首飞。这架飞机的机翼平面形状与И—350相似,但后掠角为55度,翼刀减为1个;水平尾翼安装位置上移到垂直尾翼顶部。减速板仍在机身尾部。动力装置为2台不带加力的AM—5发动机(单台最大推力19.6干牛)。武器装备为2门Н—37Д机炮。第二架原型机CM—2/2的外形开始与首架很相似,后将水平尾翼下移到了机身上,减速板前移,翼刀加高。CM—2的最
И-360 (drawing code CM-2) is the prototype of the supersonic front-line fighter. It is based on a combination of the results of the И-340 engine test and И-350's large swept wing test results based on. The first prototype CM-2/1 (Figure 1) on May 24, 1952, the first flight. The aircraft has a planar wing shape similar to И-350 but with a sweep angle of 55 degrees and a wing knife of 1, and a horizontal tail wing mounted on top of a vertical tail wing. Speedbrake is still the tail of the fuselage. The power unit is 2 AM-5 engines with no additional force (single maximum thrust of 19.6 dry cattle). Weaponry is 2 Н-37Д cannon. The second prototype CM-2/2 began with the first appearance is very similar, after the horizontal tail down to the fuselage, deceleration board forward, wing knife heightening. CM-2 most