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・ SNCAC NC.150
・ SNCAC NC.2001 Abeille
・ SNCAC NC.3021 Belphégor
・ SNCAC NC.4-10
・ SNCAC NC.510
・ SNCAC NC.860
・ SNCAIP
・ SNCAM
・ SNCAO
・ SNCAO 200
・ SNCAO 30
・ SNCAO 700
・ SNCAO CAO.600
・ SNCASE
・ SNCASE Armagnac
SNCASE Baroudeur
・ SNCASE Languedoc
・ SNCASE SE-1010
・ SNCASE SE-1210
・ SNCASE SE-2100
・ SNCASE SE-2300
・ SNCASE SE-3101
・ SNCASE SE-3110
・ SNCASE SE-400
・ SNCASE SE-700
・ SNCASE SE.100
・ SNCASE SE.200
・ SNCASE SE.212 Durandal
・ SNCASE SE.3120 Alouette
・ SNCASE SE.3200 Frelon


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SNCASE Baroudeur : ウィキペディア英語版
SNCASE Baroudeur

The SNCASE S.E.5000 Baroudeur was a French single-engined lightweight fighter designed by SNCASE (''Sud-Est'') for the NATO "Light Weight Strike Fighter" competition. An unusual design without a conventional landing gear, it used a wheeled trolley for take-off and three retractable skids to land. The Baroudeur did not enter production.
==Design and development==
The Baroudeur was a lightweight fighter, designed to operate from grass airfields. It used a wheeled trolley that could be used for take off from grass, and three retractable skids, the third at the tail for landing and for take off from snow or ice-covered surfaces. The three-wheeled trolley had provision to use rockets (two or four according to terrain plus two back-up) if needed to assist. Apart from the landing gear the aircraft was a conventional shoulder-wing monoplane with a 38 degree swept wing and tail surfaces and powered by a SNECMA Atar 101C turbojet with wing-root intakes. The first of two prototypes flew on the 1 August 1953. Three pre-production aircraft designated the S.E.5003 were also built with Atar 101D turbojet engines but the type was not ordered into production.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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