Grumman Gulfstream I

· Grumman

Airplanes

Length

19.2024 m

Flat Wing Span

23.7744 m

Height

6.7056 m

Flat Wing Area

56.6987 m²

Flat Wing Aspect Ratio

Max Seating

Cruise Speed

560.0517 km/h

Max Ceiling

10241.28 m

Number of Engines

First Flight

1958-08-14

Number Built

200

Maximum Take-Off Weight

15.9211 t (paragliders: kg)

Total Fuel Capacity

5867.388

Maximum Range

4087.734 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Grumman Gulfstream I	15.9211	5867.388	4087.734

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Saunders-Roe A.36 Lerwick		19.2024	24.384		Compare
Mikoyan MiG-110	TV7-117	18.5	22.12	49	Compare
Blackburn B-20	Rolls-Royce Vulture	21.0312	24.9936		Compare
Bréguet 500 Colmar		19.95	24.1		Compare
Aviation Traders Accountant	Rolls-Royce Dart	18.93	25.15		Compare
Douglas DC-5		18.8976	23.7744	24	Compare

All data (23 fields)

Name: Grumman Gulfstream I
Manufacturer: Grumman
Description: The Grumman Gulfstream I (company designation G-159) is a twin-turboprop business aircraft.
First Flight: 1958-08-14
Production End: 1969-01-01
Designer: Grumman
Type: Business aircraft
Length (m): 19.2024
Height (m): 6.7056
Cockpit Crew: 2
Max Seating: 24
Cruise Speed (km/h): 560.0517
Max Ceiling (m): 10241.28
Rate of Climb (m/s): 9.652
Capacity Description: 10–24 passengers / 4270 lb maximum payload
National Origin: United States of America
Number Built: 200
Powerplant Description: 2 × Rolls-Royce Dart Mk.529 or Mk.529-8E turboprop, 1633 kW (2190 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Grumman_Gulfstream_I
Flat Wing Span (m): 23.7744
Flat Wing Area (m²): 56.6987
Flat Wing Aspect Ratio: 10
Number of Engines: 2