Gulfstream Peregrine 600

Airplanes

Length

11.68 m

Flat Wing Span

10.5 m

Height

4.09 m

Max Speed

729.6874 km/h

Max Ceiling

14630.4 m

Number of Engines

First Flight

1981-05-22

Number Built

Maximum Take-Off Weight

2.812 t (paragliders: kg)

Maximum Range

2000.16 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Gulfstream Peregrine 600	2.812	2000.16

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Avtek 400A		11.99	10.67	9	Compare
FMA IAe 33 Pulqui II	Rolls-Royce Nene	11.68	10.6		Compare
AAC Wamira	Pratt & Whitney Canada PT6	10.2	11		Compare
Vought OS2U Kingfisher		10.0584	10.668		Compare
Gloster E.1/44		11.6	11		Compare
FMA I.Ae. 37	Rolls-Royce Derwent	11.78	10		Compare

All data (18 fields)

Name: Gulfstream Peregrine 600
Manufacturer: Gulfstream Aerospace
Description: The Gulfstream American Peregrine 600 was a military trainer aircraft developed in the United States in the early 1980s but which did not progress further than prototype stage.
First Flight: 1981-05-22
Designer: Gulfstream Aerospace
Length (m): 11.68
Height (m): 4.09
Cockpit Crew: 2
Max Speed (km/h): 729.6874
Min Speed (km/h): 122.2319
Max Ceiling (m): 14630.4
Rate of Climb (m/s): 26.416
National Origin: United States of America
Number Built: 1
Powerplant Description: 1 × Pratt & Whitney Canada JT15D-4 turbofan engine, 11.12 kN thrust each
Wikipedia Article (URL): en.wikipedia.org/wiki/Gulfstream_Peregrine_600
Flat Wing Span (m): 10.5
Number of Engines: 1