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Grumman C-1 Trader

The Grumman C-1 Trader (TF prior to 1962) is a carrier onboard delivery (COD) variant of the Grumman S-2 Tracker. It was replaced by a similar version of the Northrop Grumman E-2 Hawkeye, the Grumman C-2 Greyhound. It entered service in 1956 and was retired in 1988, with 87 aircraft produced.

Design and development

The C-1 Trader grew out of a need by the United States Navy for a new anti-submarine airplane. In response to this Grumman began development on a prototype twin-engine, high-wing aircraft which it designated the G-89. In 1952 the Navy designated this aircraft the XS2F-1 and flew it for the first time on December 4 that year. During the rest of the 1950s three major variants emerged, the C-1 Trader being one of them. The C-1 (originally the TF-1, for "Trainer", a secondary role)[1] was outfitted to carry nine passengers or 3,500 pounds (1,600 kg) of cargo and first flew in January 1955.

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C-1 Trader lands on USS Midway (CV-41), 1982

Throughout the 1960s and 1970s the C-1 Trader carried mail and supplies to aircraft carriers on station in the Pacific Ocean during the Vietnam War and also served as a trainer for all-weather carrier operations. Over its production life 87 C-1 Traders were built, of which four were converted into EC-1A Tracer electronic countermeasures aircraft.[2] The last C-1 was retired from USN service in 1988; it was the second-to-last radial-engine aircraft in U.S. military service (The last C-131 wasn't retired until 1990). As of 2010, approximately ten were still airworthy in civil hands, operating as warbirds.[citation needed]

In 1956 the U.S. Marine Corps Test Unit Number 1 (MCTU #1) tested the concept of using the TF-1 variant as a vehicle for inserting reconnaissance teams behind enemy lines. “On 9 July 1956 MCTU Recon Marines became the first to parachute from a TF-1. Less than three weeks later, four recon parachutists launched from the USS Bennington, which was 70 miles at sea, and jumped on a desert drop zone near El Centro California, some 100 miles inland. For the first time in Marine Corps and Naval Aviation history, the technique of introducing recon personnel off a carrier sea base to an inland objective had successfully been tested.”[3]

In August 2010, Brazilian Naval Aviation announced that it would buy and modernize eight C-1 airframes to serve in carrier onboard delivery (COD) and aerial refueling roles for use on its aircraft carrier São Paulo.[4] In 2011 contract was signed with Marsh Aviation to convert four ex-US Navy C-1A Trader airframes into KC-2 Turbo Traders.[5] The first KC-2 prototype flight was expected for November 2017 and the delivery of the first operational aircraft was scheduled for December 2018; in 2014 the contract was reaffirmed,[5] but by 2023, with no aircraft having been delivered and São Paulo long since having been stricken, the contract was cancelled.[6]

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Grumman C-1 at Willow Grove Base, Pennsylvania, USA. 1987
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On the deck of the USS Lexington, 1985
TF-1
Carrier Onboard Delivery version of the S-2 Tracker with enlarged fuselage for nine passengers, redesignated C-1A in 1962, 87 built.
TF-1Q
Electronic Countermeasures conversion of the TF-1, redesignated EC-1A in 1962, four conversions.
TF-1W
Airborne Early Warning project that was developed in the WF-2 Tracer.
C-1A
TF-1 redesignated in 1962.
EC-1A
TF-1Q redesignated in 1962.
KC-2 Turbo Trader
Marsh Aviation modernization project for Air-to-Air Refueling, requested for the Brazilian Navy.[7]
G-101
proposed 10-12 seat passenger variant
G-104
proposed tanker variant
 United States
 Brazil (Retired)
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Retired C-1 on display at an air show, 2011
Airworthy
On display
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C-1A on board USS Coral Sea, with its wings folded.

Data from Grumman aircraft since 1929.[25]

General characteristics

  • Crew: 3
  • Capacity: 9 pax / 8,500 lb (3,856 kg) payload
  • Length: 42 ft (13 m)
  • Wingspan: 69 ft 8 in (21.23 m)
  • Height: 16 ft 3.5 in (4.97 m)
  • Wing area: 485 sq ft (45.1 m2)
  • Airfoil: root: NACA 63A420; tip: NACA 63A415[26]
  • Empty weight: 16,631 lb (7,544 kg)
  • Gross weight: 23,031 lb (10,447 kg)
  • Max takeoff weight: 24,600 lb (11,158 kg)
  • Powerplant: 2 × Wright R-1820-82WA Cyclone 9-cylinder air-cooled radial piston engines, 1,525 hp (1,137 kW) each
  • Propellers: 3-bladed constant-speed fully-feathering reversible-pitch propellers

Performance

  • Maximum speed: 280 mph (450 km/h, 240 kn) at 4,000 ft (1,200 m)
  • Cruise speed: 167 mph (269 km/h, 145 kn)
  • Range: 1,110 mi (1,790 km, 960 nmi)
  • Service ceiling: 24,800 ft (7,600 m)
  • Rate of climb: 1,950 ft/min (10 m/s)
  • Wing loading: 47.5 lb/sq ft (232 kg/m2)
  • Power/mass: 0.13 hp/lb (0.21 kW/kg)

Related development

Aircraft of comparable role, configuration, and era

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