| 翻訳と辞書 |
| US Aviation CAVU ： ウィキペディア英語版 |
US Aviation CAVU
The US Aviation CAVU (named for the aeronautical meteorology term meaning "Ceiling And Visibility Unlimited") is an American high-wing, strut-braced, single-seat, open cockpit, single engine in pusher configuration, ultralight aircraft that was designed and produced by AeroDreams of Manchester, Tennessee, but marketed by US Aviation of St Paul, Minnesota under their brand name. The aircraft was supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 344. BAI Communications. ISBN 0-9636409-4-1〕〔Downey, Julia: ''1999 Kit Aircraft Directory'', Kitplanes, Volume 15, Number 12, December 1998, page 74. Primedia Publications. ISSN 0891-1851〕
==Design and development==
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The CAVU has an empty weight of . The design goals for the CAVU were a simple and inexpensive aircraft, achieving good performance with a small and inexpensive engine.〔〔
The aircraft is made from aluminium tubing, wood and fabric. The fuselage is built on an aluminium tube, which supports the tail as well as the pilot's seat. Its span wing is braced by a single lift strut. Powered by a Zenoah G-25 engine of , the CAVU cruises at . Acceptable engines can range in power from . The fuel capacity is , with optional. The landing gear is tricycle gear.〔〔
Estimated assembly time from the kit is 100 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「US Aviation CAVU」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.
|
|