Grumman C-2 Greyhound

· Grumman

Airplanes

Length

17.0688 m

Flat Wing Span

24.384 m

Height

4.572 m

Flat Wing Area

65.0321 m²

Max Seating

Cruise Speed

464.8516 km/h

Max Speed

635.2355 km/h

Max Ceiling

10210.8 m

Number of Engines

First Flight

1964-11-18

Entry Into service

1966-01-01

Number Built

Maximum Take-Off Weight

27.2155 t (paragliders: kg)

Maximum Range

2407.6 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Grumman C-2 Greyhound	27.2155	2407.6

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Grumman E-2 Hawkeye		17.3736	24.384		Compare
Saro London		17.0688	24.384		Compare
Tupolev ANT-9	Mikulin M-17	17.01	23.85	9	Compare
Douglas F6D Missileer	Pratt & Whitney TF30	16.1544	21.336		Compare
CANT Z.1011		17	25		Compare
Hütter Hü 211		16.5	24.5		Compare

All data (30 fields)

Name: Grumman C-2 Greyhound
Manufacturer: Grumman
Description: The Grumman C-2 Greyhound is a retired twin-engine, high-wing aircraft designed to carry supplies, mail and passengers to and from aircraft carriers of the United States Navy.
ICAO Code: C2
First Flight: 1964-11-18
Entry Into service: 1966-01-01
Production End: 1968-01-01
Service End: 2026-07-28
Designer: Grumman
Type: Carrier-capable transport / Carrier onboard delivery
Length (m): 17.0688
Height (m): 4.572
Cockpit Crew: 2
Max Seating: 26
Max Speed (km/h): 635.2355
Cruise Speed (km/h): 464.8516
Min Speed (km/h): 151.8639
Max Ceiling (m): 10210.8
Rate of Climb (m/s): 18.796
Capacity Description: 26 passengers / 12 litter patients / 10000 lb payload
National Origin: United States of America
Number Built: 2
Powerplant Description: 2 × Allison T56-A-425 turboprop engines, 3430 kW (4600 hp) each
Primary Users: United States Navy
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Grumman_C-2_Greyhound
Flat Wing Span (m): 24.384
Flat Wing Area (m²): 65.0321
Wake Category: M
Number of Engines: 2