Bensen Mid-Jet
| Mid-Jet | |
|---|---|
| Role | Experimental helicopter |
| National origin | United States |
| Manufacturer | Bensen Aircraft |
| Designer | Igor Bensen |
| First flight | 1953 |
| Number built | 1 |
|
| |
The Bensen Mid-Jet (a pun on "Midget jet") was a small helicopter developed by Igor Bensen in the United States in the early 1950s in the hope of attracting the interest of the United States Navy. It was a single-seat, open framework machine based on the B-5 rotor kite with small, gasoline- or fuel oil-burning ramjets mounted as tipjets on the rotor blades.[1] Tests carried out in 1954 showed it to be able to lift four times its own weight and cruise at 75 mph (120 km/h).
Specifications
General characteristics
- Crew: One pilot
- Main rotor diameter: 15 ft 0 in (4.57 m)
- Height: 5 ft 4 in (1.63 m)
- Main rotor area: 176 ft2 (16.4 m2)
- Empty weight: 100 lb (45 kg)
- Gross weight: 500 lb (227 kg)
- Powerplant: 2 × ramjets, equivalent to 20 hp (15 kW) each
Performance
- Cruise speed: 75 mph (120 km/h)
See also
- Aircraft of comparable role, configuration and era
References
 |
Wikimedia Commons has media related to Bensen aircraft. |
- Bensen Aircraft Foundation
- Lambermont, Paul Marcel (1958). Helicopters and Autogyros of the World.
- Bensen Aircraft at Vortechonline.com
- ↑ "Helicopter With 5 Pound Ramjet Engines to Fly 80 m.p.h." Popular Mechanics, June 1954, p. 138, bottom of page.
| ||||||
This article is issued from Wikipedia - version of the Tuesday, June 23, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.