原文:http://www.luft46.com/horten/ho13b.html
The Horten Ho XIII B supersonic flying wing fighter was developed from the Ho XIII A glider, which had 60 degree swept-back wings and an underslung nacelle for the pilot. The XIII B was to be powered by a single BMW 003R turbojet/rocket engine. The cockpit was located in the base of a large, sharply swept vertical fin. Like the research XIII A glider, the XIII B also had swept back wings at a 60 degree angle. Projected armament were two MG 213 20mm cannon, and the Ho XIII B was projected to be flying by mid-1946.
Span: 12 m (39' 4.8") Length: 12 m (39' 4.8") Max. Speed: 1800 km/h (1118 mph)
翻譯:
Horten Ho XIII B 超音速戰鬥機改良自Horten Ho XIII A 滑翔機其中Ho XIII A 有60度的後掠翼和斜前方的機槍給飛行員。
Ho XIII B是由一個BMW 003R渦輪噴氣發動機/火箭發動機提供動力
駕駛艙位於最大的部位,大部份位於垂直尾翼
與Horten Ho XIII A的研究相同,Ho XIII B的後掠翼也在60度角
預計裝備兩個MG213 20MM機砲還有Ho XIII B預計將在1946年年中飛行
