Top
about
element
General Info

Grumman Aerospace Grumman C-1 Trader 

General information
Type Carrier onboard delivery
National origin United States
Manufacturer Grumman
Primary user United States Navy
Number built 87
History
Introduction date 1956
First flight 19 January 1955
Retired 1988
Developed from Grumman S-2 Tracker
Developed into Grumman E-1 Tracer
.
History Grumman Aerospace
Grumman C-1 Trader Introduction date 1956
First flight 19 January 1955 Retired 1988 

The F-14 first flew on 21 December 1970 and made its first deployment in 1974 with the U.S. Navy aboard USS Enterprise (CVN-65), replacing the McDonnell Douglas F-4 Phantom II. The F-14 served as the U.S. Navy's primary maritime air superiority fighter, fleet defense interceptor, and tactical aerial reconnaissance platform into the 2000s. The Low Altitude Navigation and Targeting Infrared for Night (LANTIRN) pod system was added in the 1990s and the Tomcat began performing precision ground-attack missions

The F-14's fuselage and wings allow it to climb faster than the F-4, while the "twin-tail" empennage (dual vertical stabilizers with ventral fins on the engine nacelles) offers better stability. The F-14 is equipped with an internal 20 mm M61 Vulcan rotary cannon mounted on the left side (unlike the Phantom, which was not equipped with an internal gun in the US Navy), and can carry AIM-54 Phoenix, AIM-7 Sparrow, and AIM-9 Sidewinder anti-aircraft missiles. The twin engines are housed in widely spaced nacelles. The flat area of the fuselage between the nacelles is used to contain fuel and avionics systems, such as the wing-sweep mechanism and flight controls, as well as weaponry since the wings are not used for carrying ordnance. By itself, the fuselage provides approximately 40 to 60 percent of the F-14's aerodynamic lifting surface depending on the wing sweep position.The lifting body characteristics of the fuselage allowed one F-14 to safely land after suffering a mid-air collision that sheared off more than half of the plane's right wing in 1991

0

Km

Take off Distance

0

Km

Range

0

Km/h

Aircraft Speed

0

Max Crew

element
element
Grumman Aerospace Corporation,

Grumman Aerospace Corporation
Grumman C-1 Trader Introduction date 1956
First flight 19 January 1955 Retired 1988

1

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)
2

Powerplant

  • Empty weight: 16,631 lb (7,544 kg)
  • Gross weight: 23,031 lb (10,447 kg)
  • Max takeoff weight: (11,158 kg)
  • Powerplant: 2 × Wright R-1820-82WA Cyclone 9-cylinder air-cooled radial piston engines, 1,525 hp (1,137 kW) each
plane
3

Specifications

  • Maximum speed: 280 mph (450 km/h, 240 kn) at 4,000 ft (1,200 m)
  • Cruise speed: (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)
4

Carrier onboard delivery

Special Links Grumman C-1 Trader Introduction date 1956
First flight 19 January 1955 Retired 1988

Links to Youtube & Others

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.

Grumman Aerospace Grumman C-1 Trader

Throughout the 1960s and 1970s the C-1 Trader carried mail and supplies to aircraft carriers.

interior

Youtube Link

Carrier onboard delivery (COD) is the use of aircraft to ferry personnel, mail, supplies, and high-priority cargo.

interior
Aircrafttotal : History Grumman Aerospace, Grumman C-1A Trader

Read more in Grumman Aircraft

brand
brand
brand
brand
brand