Technical data
Technical data | HALO Gulfstream G550 |
---|---|
Length | 31 metres (including 1.6 metre nose boom) |
Height | 7.9 metres |
Wingspan | 28.5 metres |
Cabin length | 11 metres |
Cabin width | 2.24 metres |
Cabin height | 1.88 metres |
Seating capacity | 19 (normally 3 crew members and 5 to 8 scientists and engineers, depending on the instrumentation) |
Empty weight | 22.23 tonnes (49,000 pounds) |
Take-off weight | 41.28 tonnes (91,000 pounds) maximum |
Propulsion | two Rolls-Royce BR710 engines |
Thrust | 2 x 68.4 kilonewtons (15,400 pounds) |
Range | over 8000 kilometres, depending on the mission profile and payload |
Flight altitude | max. 15.5 kilometres (51,000 feet) |
Speed | max. 340 KCAS / Mach 0.885 / 1054 kilometres per hour |
Fuel capacity | 18.73 tonnes (41,300 pounds) |
Original purpose | Business jet, military usage |
DLR Flight Facility | Oberpfaffenhofen |