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René-Bonnet Missile

Bodywork

type 2S FHC
doors 2

Engine information

Bore × stroke 58.00 mm × 80.00 mm 2.28 in × 3.15 in
Cylinders S-4
Displace 0.8 litre 845 cc (51.565 cu in)
Engine type OHV
Valves 2 valves per cylinder | 8 valves in total
Engine construction
Sump
Compression ratio 9.30:1
Fuel system
Maximum power
0-50 mph
0-60 mph
0-100 mph -1.00 s
0-100 km/h
80 - 120 km/h
402 m (Quarter mile)
Standing km
Top speed 158 km/h (98 mph)
Fuel consumption
CO2 emissions
Power to weight ratio
Specific output
Maximum torque
bmep
Specific torque
Maximum rpm
Code
Main bearings
Coolant Other
Bore / stroke ratio 0.73
Unitary capacity 211.25 cc/cylinder
Aspiration Normal
Compressor type N/A
Intercooler None
Catalytic converter N

Dimensions and weight

wheelbase 2400 mm
wheelbase 94.5 in
Length (milimeters) 4100 mm
Length (inches) 161.4 in
Width (milimeters) 1499 mm
Width (inches) 59 in
Height (milimeters) 1250 mm
Height (inches) 49.2 in
L:W ratio 1.71
Ground clearance (milimeters)
Ground clearance (inches)
Kerb weight (kilograms)
Kerb weight (pounds)
Weight distribuiton
Fuel capacity (litres)
Fuel capacity (UK Ga)
Fuel capacity (US Gal)

Aerodynamics

Drag coefficient
Frontal area
Cx

Chassis

Engine location Front
Engine alignment Longitudinal
Drive FWD
Steering
Turns lock-to-lock
Turning circle
Tyres 145 x 13
Wheels
Brakes F/R Di/Dr
Brake ∅
Braked area
Transmission 4M
Top gear ratio
Final drive ratio

General information

RAC rating 8.3
Number made
Model code
Model family
Insurance classification No information available
Tax band No information available

Manual Download

Download René-Bonnet Missile PDF Manual
Designer unknown

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