Grumman Gulf Stream II
Grumman Gulf Stream II
Grumman Gulf Stream II The company developed and manufactured it. It is the first business jet in Grumman, and it is a jet aircraft that has greatly improved the turboprop machine.
It flew for the first time in 1966 and 258 aircraft were manufactured by 1979. As C-11, also VC- One machine is adopted under the name of 11A. It is used as a base to familiarize yourself with the flight characteristics. In Japan, one aircraft was adopted as a flight inspection machine (JA 8431), and it is currently being operated.
The aircraft has a jet engine on the left and right sides of the fuselage and has a T-shaped tail. The main wing is a low wing arrangement and it is a swept wing.
Essentials
- Total length: 24.36 m
- Full width: 20.98 m
- Total Height: 7.47 m
- Weight: 16.576 t
- Gross weight: 29.771 t
- Engine: Rolls-Royce Spy 511 - 8 Turbo fan (thrust 51 kN) 2 units
- Occupant: 2 people
- Passenger: Maximum 19 people
- Maximum speed: 936 km / h = M 0.76
- Range: 6,635 km
Annotation
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Post Date : 2018-01-30 15:00
This article is taken from the Japanese Wikipedia Grumman Gulf Stream II
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