| 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 |