Radne Raket 120
The Radne Raket 120 (English: Rocket) is a lightweight single cylinder, two-stroke aircraft engine used for powered hang gliders, paramotors and ultralight aircraft that is built by Radne Motor AB of Haninge, Sweden.[1][2][3][4][5]
| Raket 120 | |
|---|---|
| Type | Single cylinder, two-stroke | 
| National origin | Sweden | 
| Manufacturer | Radne Motor AB | 
| Major applications | Powered hang gliders | 
Design and development
    
The Raket 120 features electronic ignition and a Walbro carburetor. It weighs 6.8 kg (15 lb) and, due to its 13,000 rpm redline usually drives a propeller through a 3.6:1 reduction drive. The engine is equipped with a centrifugal clutch to allow running the engine without turning the propeller.[1][2][4]
Variants
    
- Raket 120 Aero
 - Model with recoil starter.[2]
 - Raket 120 Aero ES
 - Model with electric starter.[3]
 
Applications
    
- Adventure R series
 - Aerosport OY Spider
 - Airtime Explorer
 - Av8er Observer Light
 - Av8er Orbiter Lite
 - Bilsam Sky Walker
 - Blue Yonder EZ Fun Flyer
 - Dynamic Sport Rocket
 - Flylight Doodle Bug
 - Paramotor Mosquito
 - Paratour SD 120
 - Pegasus Booster
 - Rad MXL
 - Rad RXL
 - Rad SXL Custom
 - Russian Gyroplanes Gyros-1 Farmer (aux engine)
 - Russian Gyroplanes Gyros-2 Smartflier (aux engine)
 - Skyrunner Light
 - Spartan BP Parawing
 - Sperwill 120
 - Swedish Aerosport Mosquito
 - Time To Fly Racket
 - Walkerjet Spider
 - Wasp SP Mk2
 - Winds Italia Raven
 
Specifications (Raket 120 Aero)
    
Data from Radne, Wasp Systems and The World Directory of Leisure Aviation 2011-12[1][2][4]
General characteristics
    
- Type: two-stroke, single cylinder
 - Bore: 60 mm (2.4 in)
 - Stroke: 42 mm (1.7 in)
 - Displacement: 118.8 cc (7.2 cu in)
 - Length: 219 mm (8.6 in)
 - Width: 234 mm (9.2 in)
 - Height: 171 mm (6.7 in)
 - Dry weight: 6.8 kg (15 lb)
 
Components
    
- Oil system: premixed 4% oil to fuel, 25:1
 - Cooling system: air cooled
 - Reduction gear: 3.6:1 belt drive and centrifugal clutch
 
Performance
    
- Power output: 14 hp (10 kW) at 9000 rpm
 - Compression ratio: 10:1
 - Fuel consumption: 1.15 to 2 litres (0.25 to 0.44 imp gal; 0.30 to 0.53 US gal) per hour
 
References
    
- Wasp Systems (n.d.). "Radne Racket". Archived from the original on 25 April 2012. Retrieved 19 November 2011.
 - Radne Motor AB (2011). "Raket 120 Aero". Retrieved 19 November 2011.
 - Radne Motor AB (2011). "Raket 120 Aero ES". Retrieved 19 November 2011.
 - Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
 - Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 260-261. Flying Pages Europe SARL, 2015. ISSN 1368-485X
 
External links
    
    
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