Grumman G-118

Length
17.3736 m
Flat Wing Span
13.1064 m
Height
4.2672 m
Flat Wing Area
55.2773 m²
Max Mach
2 Mach
Max Ceiling
18288 m
Number of Engines
2
Aircraft Engine
Maximum Take-Off Weight
23.2312 t (paragliders: kg)
Maximum Range
2504.139 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Grumman G-118 23.2312 2504.139

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m)
McDonnell Douglas F/A-18 Hornet 17.1 12.3 Compare
McDonnell Douglas CF-18 Hornet 17.0688 12.192 Compare
Mikoyan MiG-35 17.3 12 Compare
Lockheed F-117 Nighthawk 19.812 13.1064 Compare
Avro Canada CF-103 Avro Canada Orenda 17.9832 13.1064 Compare
Lavochkin La-200 Klimov VK-1 16.351 12.96 Compare
All data (19 fields)
Name
Grumman G-118
Manufacturer
Grumman
Description
The Grumman G-118 (sometimes called the XF12F, though this was never official) was a design for an all-weather missile-armed interceptor aircraft for use on US Navy aircraft carriers.
Designer
Grumman
Type
Fighter aircraft
Length (m)
17.3736
Height (m)
4.2672
Cockpit Crew
2
Max Ceiling (m)
18288
Armament
2 x AIR-2 Genie unguided nuclear rockets or; ; 3 × AIM-7 Sparrow III missiles , or; 2 × AIM-7 Sparrow and; 3 × AIM-9 Sidewinder
Max Mach (Mach)
2
Powerplant Description
2 × J79-GE-3 after-burning turbojet engines
Primary Users
United States Navy (intended)
Status
Not built
Wikipedia Article (URL)
en.wikipedia.org/wiki/Grumman_G-118
Flat Wing Span (m)
13.1064
Flat Wing Area (m²)
55.2773
Aircraft Engine
General Electric J79
Number of Engines
2