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Rolls-Royce Soar : ウィキペディア英語版 | Rolls-Royce Soar
The Rolls-Royce RB.82 Soar, also given the Ministry of Supply designation RSr., was a small, expendable British axial-flow turbojet intended for cruise missile use and built by Rolls-Royce Limited in the 1950s. ==Design and development== The Soar was developed in the early 1950s, and was first demonstrated at the Farnborough Airshow in 1953 on each wingtip of a Gloster Meteor flying testbed. The output of the improved RB.93 Soar was 1,750 lbf (7.8 kN). As an expendable device the life of the Soar engines was limited at 10 hours.
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Rolls-Royce Soar」の詳細全文を読む
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