The HALO aircraft is based on a commercial business jet, a Gulfstream G550. The following specifications are for a production aircraft and might slightly differ from the modified HALO aircraft.
Maximum Range (8 passengers, 4 crew, NBAA IFR reserves)
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
HALO Aircraft Modifications
View ports and Apertures
Diameter: 515 mm
Diameter: 515 mm
Optical View ports
2 Top View ports
2 Bottom View ports
2 Side View ports
Diameter: 515 mm
Diameter: 515 mm
...
Top Fuselage Apertures
10 x 10"x7"
2 x 10"x14"
Bottom Fuselage Apertures
10 x 10"x7"
1 x 10"x14"
Hard points
Comment
Hard point assembly for selected aperture plates
Nose boom
1
3-D Wind field
Forward fuselage pads
6
Basis instrumentation
Unpressurized Nose compartment
30kg, 24ltr
Cabin
130kg
Stabilized Camera Platform
Cabin
Seat rails
additional seat rails on the floor and on the cabin top
Hard point on top of the tail fin
20kg
Hard points under the fuselage for Belly instrumentation pod