GRAUPNER G-BOOSTER 160 – Manual 1.91
Technical Specifications
Graupner G-Booster 160
Max. thrust:
160 N (36lb) at 15 °C (60 °F) and 1013 hPa
Diameter:
112 mm (4.4")
Length incl. starter:
288 mm (11.3")
Weight:
1450 g (3.2 lb)
Rotor speed:
30,000 – 123,000 rpm
Turbine rotor:
Inconel 70 mm (2.8")
Mass flow:
approx. 0.39 kg/s (0.86 lb/s)
Jet speed:
max. 1650 km/h (1025 mph)
Fuel consumption:
approx. 410 ml/min. (14 fl.oz/min.)
Fuel type:
Jet A1 / kerosene, approved fuel
with 5 % turbine oil, e.g. AEROSHELL 500
Maintenance interval:
50 hours or 300 million revolutions
See also 24:JET-ENGINE (page 19)
Status:
May 2006
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