| 翻訳と辞書 |
| Rogožarski SIM-Х ： ウィキペディア英語版 |
Rogožarski SIM-Х
The Rogožarski SIM-X (Serbian Cyrillic: Рогожарски СИМ-X) was a Yugoslav single-engine sports and tourist plane also used for basic training of military pilots designed in 1936, with two crew members. It was designed and built at the Rogožarski factory in Belgrade.
==Design and development==
The SIM-X was designed by Sima Milutinović at the beginning of 1936 drawing on positive experiences of its predecessors SIM-II and SIM-VIII. The prototype was designed in the Rogožarski factory from August to the end of the 1936. The first test flight took place in 1936 when the aircraft was also registered by Rogožarski factory under the code ''YU-PDY''.〔http://www.goldenyears.ukf.net/reg_YU-.htm Civil Aircraft Registar - Yugoslavija〕 After detailed test flights had been performed, it was offered to the Yugoslav air force for further tests, which were carried out at the Novi Sad school for pilots. The committee found certain minor flaws but, other than those, it was given an exceptional rating. The SIM-X which was intended for civilian use, sport pilot training, demonstration and tourist flights, was classified by the air force as "a school monoplane, two-seater for the initial training of pilots."
The SIM-X was a single engine, high monoplane parasol wing, with a wooden double-shaft propeller, for two crew members seated in tandem. Although it was envisioned that it would be possible to fit with three different engines: 120 hp Walter NZR, 110 hp Siemens and 120 hp de Havilland Gypsy Major, production aircraft were fitted with the air-cooled radial Walter NZR with a reduction gear. The engines were produced by the S. Vlajković factory Belgrade.
It was mostly of wooden construction, the elliptical cross-section fuselage was entirely made of wood and covered with plywood, and the wings were a wooden structure covered with cloth, with rounded ends. On each side, the wings were supported by a pair of inclined struts which relied on the fuselage. The fuel tank was located in the central part between the wings, that is, at their junction. Landing gear was fixed, no axles, completely made of steel pipe characterized by great strength which enabled the aircraft to land on very rugged terrain.〔Станојевић, Д.; Јанић, Ч; (12/1982.). "Животни пут и дело једног великана нашег ваздухопловства - светао пример и узор нараштајима" (in (Serbian)). Машинство (YU-Београд: Савез инжењера и техничара Југославије) 31: 1867 - 1876.〕
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「Rogožarski SIM-Х」の詳細全文を読む
スポンサード リンク
| 翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|