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Military Transport Aircraft ยทNorthrop Grumman

C-2 Greyhound

American carrier onboard delivery aircraft, commonly deployed in the late 20th century for logistics support at sea.

Origin country
๐Ÿ‡บ๐Ÿ‡ธ United States
First flight
1964Nov 18
Introduced
1966
Produced
56units
Avg unit price
$39 million
Active worldwide
26
Northrop Grumman C-2 Greyhound military transport aircraft side profile drawing
Side profile ยท Northrop Grumman C-2 Greyhound ยท length 17.1 m
Technical SpecificationsVersion: C-2A(R)
Length17.1 m (56.1 ft)
Wingspan24.6 m (80.7 ft)
Height4.9 m (15.9 ft)
Wing area65 mยฒ (699.7 sqft)
Empty weight15,307 kg (33,746 lbs)
Max. takeoff weight27,216 kg (60,001 lbs)
Powerplant2 ร— turboprops Allison T56-A-425 1,715 kW each
PerformanceVersion: C-2A(R)
Maximum speed635 km/h (395 mph)
Operational range2,400 km (1,491 mi)
Service ceiling10,211 m (33,501 ft)
Climb rate13.3 m/s (43.6 ft/s)
Operators โ€” 2026
ActiveOn order
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๐Ÿ‡บ๐Ÿ‡ธ United States

Description

The C-2 Greyhound was developed to meet the U.S. Navy's requirement for a dedicated carrier onboard delivery (COD) aircraft, replacing the piston-engine Grumman C-1 Trader. Derived from the Northrop Grumman E-2 Hawkeye, the C-2 shares the same Allison T56 turboprop engines and folding "Sto-Wings," but features a widened fuselage and a rear loading ramp optimized for efficient cargo handling. Grumman secured the production contract, with the first of two prototypes flying in 1964, leading to production commencing in 1965. A total of 17 initial C-2A aircraft were built. These aircraft underwent an overhaul in 1973 to extend their operational service life. In 1984, the Navy ordered 39 new C-2A aircraft, officially designated C-2A(R), or Reprocured C-2A, which incorporated airframe enhancements and improved avionics, including systems based on the E-2C variant.

Design

Powered by two Allison T56 turboprop engines, the C-2A is designed primarily for transport roles and does not carry offensive or defensive weaponry. It is capable of delivering up to 10,000 pounds (4,500 kg) of cargo or up to 28 passengers, typically operating with a mix of cargo and passengers. The aircraft can also be configured to accommodate litter patients for medical evacuations. A design element is the use of four vertical stabilizers, three of which are fitted with rudders. This configuration ensures adequate directional control without exceeding height restrictions for aircraft carrier hangar decks, positioning the outboard rudder surfaces directly in line with the propeller wash for effective yaw control at low airspeeds. Later upgrades to the C-2A(R) included structural improvements to the center wing, the integration of an eight-bladed NP2000 propeller, navigational system updates, crash-survivable flight-incident recorders, and a ground proximity warning system.

Operational History

Operational deployments have included logistics support for carrier strike groups. Between November 1985 and February 1987, VR-24 with its seven reprocured C-2As transported 2,000,000 pounds of cargo, 2,000,000 pounds of mail, and 14,000 passengers in the European and Mediterranean theaters. The C-2A(R) provided support to carrier battle groups during Operation Desert Shield, Desert Storm, and Operation Enduring Freedom. In June 2011, two C-2A(R) Greyhounds were loaned to the French Navy to support logistics for the aircraft carrier Charles de Gaulle during the NATO intervention in Libya, returning to U.S. control after 16 days. The CMV-22B Osprey progressively took over the carrier onboard delivery mission from 2020. VRC-30 was decommissioned in 2023, leaving VRC-40 as the last COD squadron; the type's final arrested landing and catapult launch took place aboard USS Nimitz on 25 June 2026 during FLEETEX 250. VRC-40 was disestablished at Naval Station Norfolk on 23 July 2026, retiring the C-2A after six decades of service, and the last airframe was flown to the National Naval Aviation Museum in Pensacola, Florida.

Variants

Main Variants:

  • YC-2A: The prototype variant, converted from E-2A Hawkeyes, featured a redesigned fuselage.

  • C-2A: This was the initial production variant of the Greyhound, with a total of 17 aircraft built.

  • C-2A(R): Known as the "Reprocured" C-2A, this version incorporated improved systems based on the E-2C variant.

  • Greyhound 21: A concept only, this turbofan-powered variant was proposed for various roles, including anti-submarine warfare, electronic warfare, electronic surveillance, carrier onboard delivery, and aerial refueling.

Frequently Asked Questions

What type of aircraft is the C-2 Greyhound?
The Northrop Grumman C-2 Greyhound is a military transport aircraft aircraft developed by Northrop Grumman and entered service in 1966.
What is the maximum speed of the C-2 Greyhound?
The Northrop Grumman C-2 Greyhound has a maximum speed of 635 km/h (394 mph).
What is the range of the C-2 Greyhound?
The Northrop Grumman C-2 Greyhound has an operational range of 2,400 km (1,491 miles). This range can vary based on payload, altitude, and mission profile.
When did the C-2 Greyhound first fly?
The Northrop Grumman C-2 Greyhound made its first flight on November 18, 1964. It entered operational service in 1966.
How many C-2 Greyhound have been built?
Approximately 56 units of the Northrop Grumman C-2 Greyhound have been produced since it entered service in 1966.
Which countries operate the C-2 Greyhound?
The Northrop Grumman C-2 Greyhound is operated by 1 countries with approximately 26 aircraft in active service. The largest operators include United States.
How much does a C-2 Greyhound cost?
The Northrop Grumman C-2 Greyhound has an estimated unit cost of approximately $39.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the C-2 Greyhound?
The Northrop Grumman C-2 Greyhound has a service ceiling of 10,211 meters (33,500 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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