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BRM Aero Bristell NG 5

brm-ng5


The BRM Aero Bristell is a Czech low-wing, two-seat in side-by-side configuration, single engine in tractor configuration, ultralight and light-sport aircraft that was designed by Milan Bristela and produced by BRM Aero. The aircraft was supplied as a complete ready-to-fly aircraft.

The aircraft was designed to comply with both European microlight rules and also the US light-sport aircraft regulations, by using different versions for each regulatory environment.

The aircraft is made from aluminium and features a 130 cm (51 in) wide cabin at the shoulder, with a bubble canopy over the cockpit. The wings feature flaps. The standard engine is a 60 kW (80 hp) Rotax 912UL, with the 75 kW (101 hp) Rotax 912ULS, the 71 kW (95 hp) ULPower UL260i/iS and the 88 kW (118 hp) ULPower UL350iS powerplants optional. The 115 hp (86 kW) Rotax 914, 85 hp (63 kW) Jabiru 2200 and 120 hp (89 kW) Jabiru 3300 are also available. Other engines are planned, particularly for the United States market. The aircraft has a useful load of 279 kg (615 lb). The landing gear is of tricycle configuration.

The aircraft was introduced at the Aero show held in Friedrichshafen in 2011. After 42 examples had been completed  (September 2011) the aircraft was introduced into the US market in September 2011 at the AOPA Summit. The 2011 base price was US$125,000.

Ultralight aeroplane Bristell UL and its modifications Bristell HD, Bristell RG and Bristell LSA are aeroplanes for flight training in flight schools, gliders towing and recreational flying.
The Bristell HD version offers heavy-duty wing spars, and Bristell RG is a version with retractable undercarriage.

 

The Bristell tricycle-gear (and new taildragger version), low-wing S-LSA comes standard with 10-inch Dynon SkyView or Advance Flight Systems AF5600 EFIS panel, Com, two-axis autopilot, BRS parachute and leather interior. Price 2012: $156,000.
 

Bristell-NG5

 

Variants:

Bristell UL
Base ultralight model
Engine: 1 × Rotax 912ULS , 75 kW (100 hp)
Wing span: 8,13 m (26 ft 8 in)
Wing area: 10,5 sq.m (113 sq ft)
Wing loading: 45 kg/ sq.m
Length: 6,45 m (21 ft 2 in)
Height: 2,28 m (7 ft 6 in)
Cabin width: 1,3 m
Empty weight: 290 kg (639 lb)
Maximum take-off weight: 472,5 kg (1,042 lb)
Useful load: 182,5 kg
Fuel tanks capacity: 130 lt (29 imp gal; 34 US gal)
Fuselage luggage compartment: 15 kg
Wing luggage compartment: 2 x 20 kg
Load factors: +4/-2g
Stall speed with flaps VSO: 52 km/h
Stall speed without flaps Vs1: 67 km/h
Manoeuvring speed VA: 165 km/h
Maximum flap speed VF: 139 km/h
Cruising speed: 214 km/h     250 km/h
Never exceeded speed VNE: 270 km/h
Seats: 2

Bristell HD
Heavy duty model
Wing span: 8,13 m
Wing area: 10,5 sq.m
Wing loading: 57,1 kg/ sq.m
Length: 6,45 m
Height: 2,28 m
Cabin width: 1,3 m
Empty weight: 310 kg
Maximum take-off weight: 600 kg
Useful load: 290 kg
Fuel tanks capacity: 130 lt
Fuselage luggage compartment: 15 kg
Wing luggage compartment: 2 x 20 kg
Load factors: +4/-2g
Stall speed with flaps VSO: 78 km/h
Stall speed without flaps Vs1: 87 km/h
Manoeuvring speed VA: 165 km/h
Maximum flap speed VF: 139 km/h
Cruising speed: 250 km/h
Never exceeded speed VNE: 290 km/h

Bristell LSA
Model for the US light-sport aircraft category
Wing span: 9,13 m
Wing area: 11,75 sq.m
Wing loading: 51,06 kg/sq.m
Length: 6,45 m
Height: 2,28 m
Cabin width: 1,3 m
Empty weight: 330 kg
Maximum take-off weight: 600 kg     
Useful load: 270 kg
Fuel capacity: 130 lt
Fuselage luggage capacity: 15 kg
Wing luggage compartment: 2 x 20 kg
Load factors: +4/-2g
Stall speed with flaps VSO: 58 km/h
Stall speed without flaps Vs1: 74 km/h
Manoeuvring speed VA: 165 km/h
Maximum flap speed VF: 139 km/h
Cruising speed: 250 km/h     
Never exceeded speed VNE: 290 km/h     

Bristell RG
Rectractable gear model
Wing span: 9,13 m (30.0 ft)
Wing area: 11,75 sq.m
Wing loading: 51,06 kg/ sq.m
Length: 6,45 m
Height: 2,28 m
Cabin width: 1,3 m
Empty weight: 335 kg
Maximum take-off weight: 600 kg (1,323 lb)
Useful load: 265 kg
Fuel tanks capacity: 130 lt
Fuselage luggage compartment: 15 kg
Wing luggage compartment: 2 x 20 kg
Load factors: +4/-2g
Stall speed with flaps VSO: 58 km/h
Stall speed without flaps Vs1: 74 km/h
Manoeuvring speed VA: 165 km/h
Maximum flap speed VF: 139 km/h
Cruising speed: 250 km/h
Never exceeded speed VNE: 290 km/h

 

 


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