| タイトル | Aerocrane: A hybrid LTA aircraft for aerial crane applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760007975 |
| 著者（英） | Doolittle, D. B.; Perkins, R. G., Jr. |
| 著者所属（英） | Naval Air Systems Command |
| 発行日 | 1975-01-01 |
| 言語 | eng |
| 内容記述 | The Aerocrane, a hybrid aircraft, combines rotor lift with buoyant lift to offer VTOL load capability greatly in excess of helicopter technology while eliminating the airship problem of ballast transfer. In addition, the Aerocrane concept sharply reduces the mooring problem of airships and provides 360 deg vectorable thrust to supply a relatively large force component for control of gust loads. Designed for use in short range, ultra heavy lift missions, the Aerocrane operates in a performance envelope unsuitable for either helicopters or airships. Basic design considerations and potential problem areas of the concept are addressed. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 76N15063 |
| 権利 | No Copyright |
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