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C-160 Transall

C-160 Transall

Military Transport Aircrafts
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Basic Information
Name
C-160 Transall
Designation
C-160 Transall
Alternate Designation
C-160D (German version), C-160F (French version), C-160G Gabriel (Sigint version), C-160H Astarte (submarine commucations relay version), C-160NG, C-160T (Turkish version), C-160Z (South African version)
Equipment Type
Military Transport Aircrafts
Manufacturer
Transall Allianz
Date of Introduction
1967
Description

The C-160 Transall is a tactical military transport aircraft developed in partnership 50/50 by France and Germany in the 1960s through the Transall Allianz consortium. The first prototype took to the air in 1963 followed by first deliveries in 1967. Production ceased in 1972 with 169 aircraft delivered to Germany (110), France (50) and South Africa (9). Production was restarted between 1981 and 1985 to deliver 33 C-160NG (Next-Generation) to France (29) and Indonesia (4). Turkey took delivery of 20 ex-German C-160s. The surviving aircraft in German and French air forces were upgraded in the 1990s to extend their service life until their replacement by the Airbus A400M aircraft. The C-160 aircraft is powered by two Rolls-Royce Tyne turboprops, each rated at 6,000-shp, driving four-bladed propellers. The aircraft is able to transport a 16t payload at ranges of 1,800 km or an eight-ton payload at ranges of 5,000 kilometers. The C-160 can transport personnel, equipment, military vehicles, artillery and paratroops. The C-160G Gabriel is a Signals Intelligence (SIGINT) variant. C-160H Astarte is a submarine communications relay aircraft utilized by the French Navy. The upgraded C-160NG features a fixed refueling probe and can be converted to air refueling tanker aircraft.

Air & Air Defense Specifications
Crew 3
Max Speed 513.0 km/h
Range 1853.0 km
Service Ceiling 8230 m
Wingspan 40.00 m
Overview (Deagel)
Group Military Transport Aircrafts
Status Active
Also Known As C-160D (German version), C-160F (French version), C-160G Gabriel (Sigint version), C-160H Astarte (submarine commucations relay version), C-160NG, C-160T (Turkish version), C-160Z (South African version)
Origin France, Germany
Initial Operational Capability (IOC) 1967
First Flight February 25, 1963
Total Production 202
Specifications (Deagel)
Crew 3
Number of Engines 2
Paratroops 68
Propeller Blades 4
Stretchers 62
Troops 93
Area — Wing Area 160 square meter
Dimensions — Height 11.7 meter
Dimensions — Length 32.4 meter
Dimensions — Wingspan 40 meter
Mass — Cargo 16 ton
Mass — Max Takeoff Weight 51,000 kilogram
Mass — Operational Weight 29,000 kilogram
Performance — Ceiling 27,000 foot
Performance — Ferry Range 8,850 kilometer
Performance — Max Range 1,853 kilometer
Performance — Take Off Run Distance 715 meter
Power — Max Power at TakeOff 12,000 shp
Speed — Climb Rate 1,300 fpm
Speed — Top Speed at High Altitude 513 kph
Details
Country of Origin France
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
32.4 m
Width
40 m
Height
11.7 m
Weight
51000 kg
Operators (5)
France
Germany
Turkey
South Africa
Indonesia
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