Dynamic Sport Rocket
| Rocket | |
|---|---|
| Role | Paramotor |
| National origin | Poland |
| Manufacturer | Dynamic Sport |
| Status | Production completed |
The Dynamic Sport Rocket is a series of Polish paramotors designed and produced by Dynamic Sport of Kielce for powered paragliding. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1]
Design and development
The Rocket was designed to comply with the US
paraglider-style wing, single-place accommodation and a single Radne Raket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 100 to 120 cm (39 to 47 in) diameter propeller, depending on the model. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal), with 10 litres (2.2 imp gal; 2.6 US gal) optional.[1]
As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]
Variants
- Rocket 100
- Model with a Radne Raket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 100 cm (39 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal).[1]
- Rocket 110
- Model with a Radne Racket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 110 cm (43 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal; 2.6 US gal).[1]
- Rocket 115
- Model with a Radne Racket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 115 cm (45 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal; 2.6 US gal).[1]
- Rocket 120
- Model with a Radne Racket 120 14 hp (10 kW) engine in pusher configuration with a 3.25:1 ratio reduction drive and a 120 cm (47 in) diameter propeller. The fuel tank capacity is 5 litres (1.1 imp gal; 1.3 US gal) or optionally 10 litres (2.2 imp gal; 2.6 US gal).[1]
Specifications (Rocket 100)
Data from Bertrand[1]
General characteristics
- Crew: one
- Empty weight: 17 kg (37 lb)
- Fuel capacity: 5 litres (1.1 imp gal; 1.3 US gal)
- Powerplant: 1 × two-stroke, air-cooled aircraft engine, with a 3.25:1 reduction drive
- Propellers: 2-bladed fixed pitch, 1.00 m (3 ft 3 in) diameter