Tech­ni­cal da­ta

Modifications - from business jet to research aircraft
Mod­i­fi­ca­tions - from busi­ness jet to re­search air­craft
Credit: DLR (CC-BY 3.0)

Modifications - from business jet to research aircraft

Mod­i­fi­ca­tions - from busi­ness jet to re­search air­craft

HALO Gulfstream G550 technical data

Length31 metres (including 1.6 metre nose boom)
Height7.9 metres
Wingspan28.5 metres
Cabin length11 metres
Cabin width2.24 metres
Cabin height1.88 metres
Seating capacity19 (normally 3 crew members and 5 to 8 scientists
and engineers, depending on the instrumentation)
Empty weight22.23 tonnes (49,000 pounds)
Take-off weight41.28 tonnes (91,000 pounds) maximum
Propulsiontwo Rolls-Royce BR710 engines
Thrust2 x 68.4 kilonewtons (15,400 pounds)
Rangeover 8000 kilometres, depending on the mission profile
and payload
Flight altitudemaximum 15.5 kilometres (51,000 feet)
Speedmaximum 340 KCAS / Mach 0.885 / 1054 kilometres per hour
Fuel capacity18.73 tonnes (41,300 pounds)
Original purposeBusiness jet, military usage
DLR Flight FacilityOberpfaffenhofen

Contact
  • Falk Dambowsky
    Ed­i­tor
    Ger­man Aerospace Cen­ter (DLR)
    Me­dia Re­la­tions
    Com­mu­ni­ca­tions and Me­dia Re­la­tions
    Telephone: +49 2203 601-3959
    Fax: +49 2203 601-3249
    Linder Höhe
    51147 Cologne
    Contact
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