File:Rotorway Scorpion Too (2909011406).jpg
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DescriptionRotorway Scorpion Too (2909011406).jpg | The Scorpion Too consisted of aluminum components mounted on a truss-frame, steel tube tail boom attached to a steel-tube fuselage enclosed by a smooth Fiberglas shell. A builder or pilot could remove the shell for easier access to internal equipment. Schramm and Everts based the Scorpion Too main rotor blade design on the two-blade, teetering system pioneered by Arthur Young on the Bell Model 30 helicopter (see NASM collection). Young's design was simple and lightweight. The most novel technical feature on the Scorpion series was the method used to transmit engine power to the tail rotor. Three V-belts coupled the long shaft turning inside the tail boom to the engine drive shaft and final tail rotor drive shaft. Nearly all helicopters used gear boxes to step the power from one shaft to the next but the Scorpion Too could not afford the weight penalty of heavy gears turning inside metal boxes filled with lubricating fluid. A standard drive shaft was not compatible with the lightweight structure of the aircraft, as it was too light to withstand the vibrations generated by the rotor system. |
Date | |
Source |
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Author | Cliff from I now live in Arlington, VA (Outside Washington DC), USA |
Camera location | 38° 54′ 39.23″ N, 77° 26′ 34.83″ W | View this and other nearby images on: OpenStreetMap | 38.910896; -77.443008 |
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[edit]This file is licensed under the Creative Commons Attribution 2.0 Generic license.
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This image, originally posted to Flickr, was reviewed on July 26, 2009 by the administrator or reviewer File Upload Bot (Magnus Manske), who confirmed that it was available on Flickr under the stated license on that date. |
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 10:05, 26 July 2009 | 1,280 × 853 (400 KB) | File Upload Bot (Magnus Manske) (talk | contribs) | {{Information |Description= The Scorpion Too consisted of aluminum components mounted on a truss-frame, steel tube tail boom attached to a steel-tube fuselage enclosed by a smooth Fiberglas shell. A builder or pilot could remove the shell for easier acce |
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Camera manufacturer | Canon |
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Camera model | Canon EOS 5D |
Exposure time | 1/60 sec (0.016666666666667) |
F-number | f/3.5 |
ISO speed rating | 400 |
Date and time of data generation | 16:01, 25 May 2008 |
Lens focal length | 52 mm |
Orientation | Normal |
Horizontal resolution | 72 dpi |
Vertical resolution | 72 dpi |
Software used | ACD Systems Digital Imaging |
File change date and time | 22:58, 2 October 2008 |
Y and C positioning | Centered |
Exposure Program | Not defined |
Exif version | 2.2 |
Date and time of digitizing | 16:01, 25 May 2008 |
APEX shutter speed | 6 |
APEX aperture | 3.625 |
APEX exposure bias | 0 |
Metering mode | Pattern |
Flash | Flash did not fire, compulsory flash suppression |
DateTime subseconds | 281 |
Color space | sRGB |
Focal plane X resolution | 3,086.925795053 |
Focal plane Y resolution | 3,091.2951167728 |
Focal plane resolution unit | inches |
Custom image processing | Normal process |
Exposure mode | Auto exposure |
White balance | Auto white balance |
Scene capture type | Standard |