High Quality Content by WIKIPEDIA articles! Unlike in earlier projects, the Imperial Japanese Army issued in February 1936 detailed specifications that had to be met by the new aircraft. These included a maximum speed 399 km/h (248 mph) at 3,000 m (9,840 ft); climb to altitude in under eight minutes; take-off in less than 300 m (980 ft); normal operating altitude from 2,000 m (6,560 ft) to 4,000 m (13,120 ft); and endurance of more than five hours at 299 km/h (186 mph) at 3,000 m (9,840 ft). Structural strength was specified as well, including a load factor of 6 while at high angle of attack, and 4 while in a glide. Minimum bombload for short-range missions was to be 1,500 kg (3,310 lb) with a variety of load configurations. Loaded, the bomber was to have a weight of less than 1,000 kg (2,200 lb). Other specified requirements were a crew of from four to six; engines to be either the Nakajima Ha-5 or Mitsubishi Ha-6; and three gun positions (nose, dorsal and ventral, each with one flexible 7.7 mm (0.303 in) Type 89 machine gun). The Hi-2 (Type 94) or Hi-5 radio, and other details were also specified.

Данное издание не является оригинальным. Книга печатается по технологии принт-он-деманд после получения заказа.