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Ki-21 "Sally"
The first prototype Ki-21 flew on December 18, 1936. The Ki-21 was a midwing plane with X-6 Kinsei (Gold Star) engines with Hamilton Standard three-blade variable pitch propellers. The three-spar wing had a working light alloy skin and was divided into three sections. The ailerons were made of light alloy with fabric sheathing. Hydraulically extendable flaps are all metal. The semi-monocoque fuselage with a working skin had an oval cross-section. The bomb bay was located under the spars of the center section, and above them were two gas tanks, shifted to the left side (there was a passage to the tail section on the right). The plumage had a metal structure with linen sheathing. The first and second pilot-navigator were located side by side, the bombardier was in the bow, the gunner-radio operator was in the tail. Defensive armament consisted of three 7.7-mm Type-89 machine guns. One was in the bow turret with firing angles only in the vertical plane, the second was in the rear turret, and the third was in the lower hatch. The chassis was retracted and released hydraulically. The first production Ki-21-1a did not look different from the third prototype. The engines Ha-5 - "army type 97" with a capacity of 950 liters were chosen as the power plant. with. at 2400 rpm at sea level and 1080 hp. with. at an altitude of 4000 m. The fuel supply was increased from 1840 liters to 2635 liters. Defensive armament consisted of three 7.7 mm machine guns. Type 97 Model I Bombers of Hamamatsu Army Flying School
Modifications
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