To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.

From Wikipedia, the free encyclopedia

Role Target drone
National origin France
Manufacturer Nord Aviation
First flight c.1959
Introduction 1960
Retired 1971 (U.S. Navy)
Primary users French Air Force
United States Navy
Number built 62

The Nord CT.41 Narwhal was a French target drone, designed and built by Nord Aviation during the late 1950s for the purpose of providing training in the interception of supersonic bomber aircraft.

Design and development

Starting development in 1957, the CT.41 used a canard configuration, with a short, straight wing located at mid-fuselage with wingtip-mounted ramjet engines.[1] Launched using an elevating ramp,[2] two solid rocket boosters provided initial thrust upon launch, with the ramjets igniting at a speed of Mach 1.7.[3] Command guidance was used for control; the aircraft could be fitted with electronic enhancers and flares to boost its target signature.[3] Two types were produced, the CT.41A for high-altitude use, and the CT.41B for low-altitude training. If the drone was not shot down, recovery was via parachute.[3]


Operational history

The CT.41 began test flights during 1959,[2] with production starting later that year; 62 aircraft were constructed for use by the French Air Force. They had only a brief service life before being retired due to being too fast to provide practical training for interceptor pilots. Hawker Siddeley acquired a manufacturing license for the type in November 1960.[2] Six were acquired by Bell Aircraft for evaluation by the United States Navy; Bell also acquired a production license for the type, which in 1962 received the U.S. designation PQM-56A. The PQM-56A was out of service by the early 1970s.[3]


Data from Directory of U.S. Military Rockets and Missiles (2003)[1][3]

General characteristics

  • Crew: None
  • Length: 9.80 m (32 ft 2 in)
  • Wingspan: 3.73 m (12 ft 3 in)
  • Height: 2.18 m (7 ft 2 in)
  • Gross weight: 1,297 kg (2,860 lb)
  • Max takeoff weight: 2,550 kg (5,622 lb) with boosters
  • Powerplant: 2 × Type 625 ramjet


  • Maximum speed: Mach 3.1
  • Endurance: 14 minutes
  • Service ceiling: 20,000 m (65,000 ft)



  1. ^ a b "The 23rd Paris Show". Flight, 14 August 1959. p.20.
  2. ^ a b c "Nord C.T.41". Flight, 12 August 1960, p.215.
  3. ^ a b c d e Parsch 2003


  • Parsch, Andreas (2003). "Nord/Bell CT.41/PQM-56". Directory of U.S. Military Rockets and Missiles. Retrieved 2014-05-09.
This page was last edited on 1 February 2021, at 14:47
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.