Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Nord CT41

From Wikipedia, the free encyclopedia
French supersonic target drone
CT41
PQM-56
RoleTarget drone
Type of aircraft
National originFrance
ManufacturerNord Aviation
First flightc.1959
Introduction1960
Retired1971 (U.S. Navy)
Primary usersFrench Air Force
United States Navy
Number built62

TheNord CT.41 Narwhal was a Frenchtarget drone, designed and built byNord Aviation during the late 1950s for the purpose of providing training in the interception of supersonic bomber aircraft.

Design and development

[edit]

Starting development in 1957, the CT.41 used acanard configuration, with a short, straight wing located at mid-fuselage with wingtip-mounted ramjet engines.[1] Launched using an elevating ramp,[2] twosolid rocket boosters provided initial thrust upon launch, with the ramjets igniting at a speed ofMach 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

[edit]

The CT.41 began test flights during 1959,[2] with production starting later that year; 62 aircraft were constructed for use by theFrench 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 amanufacturing license for the type in November 1960.[2] Six were acquired byBell Aircraft for evaluation by theUnited States Navy; Bell also acquired a production license for the type, which in 1962 received the U.S. designationPQM-56A. The PQM-56A was out of service by the early 1970s.[3]

Specifications

[edit]

Data fromDirectory 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 625ramjet

Performance

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

References

[edit]
Wikimedia Commons has media related toCT.41.

Citations

[edit]
  1. ^ab"The 23rd Paris Show".Flight, 14 August 1959. p.20.
  2. ^abc"Nord C.T.41".Flight, 12 August 1960, p.215.
  3. ^abcdeParsch 2003

Bibliography

[edit]
  • Parsch, Andreas (2003)."Nord/Bell CT.41/PQM-56".Directory of U.S. Military Rockets and Missiles. designation-systems.net. Retrieved2014-05-09.
Manufacturer
designations
By role
Light transport
Trainers
Army Observation
Maritime patrol
Research
Target drones
Transports
Helicopters
Missiles
Manufacturer
designations
Fighter aircraft
Target drones
Attack helicopters
Observation and
utility helicopters
Commercial helicopters
Tiltrotors
UAVs
Non-production helicopters
Experimental aircraft
Names
1 Unknown/not assigned
1–50
51–100
101–150
151–200
201–
Undesignated
Retrieved from "https://en.wikipedia.org/w/index.php?title=Nord_CT41&oldid=1162175215"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp