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G550 Specifications
The HALO aircraft is based on a commercial business jet, a Gulfstream G550.
More information about Gulfstream and the G550 is available at the
Gulfstream website.
The following specifications are for a production aircraft. The actual specifications
of the modified HALO aircraft are somewhat different from the data of the production aircraft.
| Aircraft Performance |
Maximum Range
(8 passengers, 4 crew, NBAA IFR reserves)
The actual range will also be affected by speed, weather, outfitting options and others.
|
12,501 km at Mach 0.8
|
| Maximum Operating Mach Number | Mach 0.885 |
| Takeoff Distance (SL, ISA, MTOW) | 1,801 m |
| Landing Distance (SL, ISA, MLW) | 844 m |
| Maximum Cruise Altitude | 15,545 m |
| Weights |
| Maximum Takeoff Weight | 41,277 kg |
| Maximum Landing Weight | 34,156 kg |
| Maximum Zero Fuel Weight | 24,721 kg |
| Maximum Payload | 2,812 kg |
| Payload with Maximum Fuel | 816 kg |
| Design Standards |
| Rolls-Royce BR710 Engines | 2 |
| Maximum Passengers | 19 |
| Exterior |
| Length | 29.4 m |
| Height | 7.9 m |
| Wingspan | 28.5 m |
| Interior |
| Cabin Length | 15.3 m |
| Cabin Height | 1.88 m |
| Cabin Width | 2.24 m |
| Cabin Volume | 47.3 m3 |
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