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Nord Aviation CT20

Military Aircraft

The Nord CT20 was a French radio-controlled target drone introduced in 1957 and built by Nord Aviation. It grew out of the Arsenal and SFECMAS T.5.510 design, was powered by a Turbomeca Marboré II turbojet and could reach about 900 kilometres per hour for a flight of 55 to 60 minutes. It took off from a ramp with the help of two rockets, was flown by radio signals from the ground and, being made of light material, floated, so a drone that came down on water could be recovered. Variants included the R20 battlefield reconnaissance drone, 62 of which were built for the French Army, and the Swedish Saab Rb 08 anti-ship missile. It was also used to help develop air-to-air missiles.

Facts
Year
1957 1
Engine Class
Turbojet 1
Top Speed (km/h)
900 1
Mass (kg)
490 1
Maximum Mass (kg)
660 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Nord Aviation CT20 (Wikipedia)

Of Make

Source Nord Aviation CT20 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Nord Aviation CT20 (Wikipedia)Lead, maker
Quote, Lead, maker
the CT.20 was built by Nord Aviation and powered by a Turbomeca Marboré II engine

Originated In

Also in Geography Atlas: where this subject originated.

Source Nord Aviation CT20 (Wikipedia)Lead, origin
Quote, Lead, origin
The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957
Sources
1. Nord Aviation CT20 (Wikipedia)
  • Lead, introduction
    The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957
  • Lead, type
    The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957
  • Lead, engine
    The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957
  • Lead, top speed
    providing a top speed of 900 km/h (560 mph; 490 kn)
  • Specifications, empty weight
    Empty weight: 490 kg (1,080 lb)
  • Specifications, maximum take-off weight
    Max takeoff weight: 660 kg (1,455 lb)
  • Lead, maker
    the CT.20 was built by Nord Aviation and powered by a Turbomeca Marboré II engine
  • Lead, origin
    The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957
  • Exemplifies: Aviation, Lead, mode
    The Nord Aviation CT20 was a French turbojet-powered radio-controlled target drone introduced in 1957
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