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.
Design and development
The Rocket was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a 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.
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.
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).
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).
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).
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).
Data from Bertrand
General characteristics
Crew: one
Empty weight: 17 kg (37 lb)
Fuel capacity: 5 litres (1.1 imp gal; 1.3 US gal)
Powerplant: 1 × Radne Raket 120 single cylinder, 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
