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Canadair CL-89

The Canadair CL-89 is a surveillance drone (UAV) produced jointly by Canada, Britain and West Germany in the 1960s. A larger and improved model with a greater payload, the CL-289, was later introduced.

CL-89
A German Army CL-289
Role Surveillance drone
National origin Canada
Manufacturer Canadair
First flight March 1964

History edit

CL-89 edit

 
Cl-89 NATO AN USD-501

In June 1963, a sponsorship by Canada and Britain[1][2] agreed to have Canadair design, evaluate and test the CL-89 drone. The concept had been developed at Canadair from the CL-85, a study for the carriage of dispatches. West Germany later joined the group,[3] and although the United States was invited to join, they declined.[citation needed]

The first, less than successful flight was made at Yuma, Arizona in March 1964. The British wanted changes in the system (consisting of the drone, the launcher, the retrieval equipment and the support) to be "Soldier Proof". They sent an army officer to Canadair and with his help set up a maintenance advisory group which had excellent results. CL-89 had a difficult development and was almost abandoned.[citation needed]

The first complete CL-89 system was supplied to the West Germans in 1969. During the 1970s, Both France and Italy joined the British and West Germans in operating the CL-89. NATO gave the entire system the designation AN/USD-501 (Army Navy Unmanned Surveillance Drone type 501); in UK service it was known as the Midge (Military Intelligence & Data Gathering Equipment). The system was designed for information collecting at a divisional level.

In Royal Artillery service Midge was operated by a troop in a divisional locating battery. This troop had two launchers, all the facilities for processing and analysing imagery and for repair and servicing of the aircraft. The troop comprised two officers and about 70 soldiers. Tasking was through the artillery intelligence cell at divisional HQ and the primary use was to confirm suspected enemy locations, particularly hostile artillery. In UK service Midge replaced the Northrop Radioplane SD-1, known in service as "Observer", and was replaced in turn by Phoenix. Midge was used operationally in Kuwait in 1991, with some effect especially when combined with artillery raids.

In German Army service, CL-89 was operated by a battery in the divisional observation battalion. The organisation was similar to the British but had six officers and about 120 soldiers.

Logistic support for CL-89 was provided to user nations through NAMSA.

CL-289 edit

 
CL-289 NATO AN USD 502

In November 1987, an agreement was signed between Canada, West Germany and France for the production of the CL-289 system. The design of this was started in 1974. It was a larger drone with better range and payload than the CL-89. It was intended to obtain corps level intelligence for the armies of NATO. Although similar in appearance to the CL-89, many changes in design were necessary. The CL-289 entered service in November 1990, the entire system being designated AN/USD-502. At least 9 CL-289 were shot down by the Yugoslavian National Army during the NATO aggression on Yugoslavia in 1999.

Description edit

The cylindrical body had four stub-wings at the rear of the fuselage, with aerodynamic trim provided by smaller canard foreplanes.

Although the drone looked and flew like a missile and was launched from truck-mounted rails, it cruised under jet power. Takeoff was achieved by a booster rocket, which was jettisoned when flight speed was attained. A small turbojet then took over for the rest of the flight

The flight pattern was programmed and allowed for the flight to the target areas, a run while the cameras or sensors recorded, and the return to the recovery site. On arrival at this calculated position, the motor cut and a drogue parachute was deployed. This slowed the drone down sufficiently to alter its attitude and allow a parachute to be released from the underside of the drone causing it to invert. Before reaching the ground a pair of pneumatic landing bags were released from the top of the drone (now facing the ground). The retrieval crew would then remove the cameras etc., and return the drone to be ready for its next flight. A camera or sensor, dependent on the mission, could be fitted to the CL-89, and multiple units to the CL-289.

Being a drone meant that it flew a programmed course and was not under any form of external control. In the CL-89 the programmed flight path was constrained by the very limited number of 'events' that could be programmed. These events including turns, changes in altitude, sensor activations/de-activations and landing. The programmed flightpath had to be corrected for meteorological conditions. Data for this was provided by a standard artillery Target Acquisition meteor message.

Two types of sensors were used with the CL-89, both using photographic film that was processed and analysed after the drone was recovered. Standard black and white film was normally used in daylight, with flares available for night use. Infrared linescan, an early form of thermal imaging was generally used at night. Three types of sensors were used with the British Drone Troops, Vinten (day sensor), Zeiss (day and night) and IRLS (day and night).

Operators edit

  Canada
  France
  Germany
  Italy
  Turkey
  United Kingdom

Specifications edit

Data from Jane's All the World's Aircraft 1982-83 [5]

General characteristics

  • Length: 12 ft 2 in (3.71 m) (with booster)
  • Wingspan: 3 ft 1 in (0.94 m)
  • Diameter: 1 ft 1 in (0.33 m) (body diameter)
  • Empty weight: 172.4 lb (78 kg)
  • Max takeoff weight: 343 lb (156 kg) (with booster)
  • Powerplant: 1 × Williams International WR2-6 turbojet, 125 lbf (0.56 kN) thrust
  • Powerplant: 1 × BAJ Vickers Wagtail rocket booster, 5,000 lbf (22 kN) thrust

Performance

  • Maximum speed: 460 mph (740 km/h, 400 kn)
  • Range: 37 mi (60 km, 32 nmi)
  • Service ceiling: 10,000 ft (3,000 m)

See also edit

Related lists

References edit

  1. ^ "Defence". 2012-11-03 at the Wayback Machine Flight International, 29 April 1965, Volume 87, No. 2929. p. 683.
  2. ^ "Missiles and Spaceflight: Canadair Cl-89". 2012-11-03 at the Wayback Machine Flight International, 25 June 1964, Volume 85, Number 2885. p. 1082.
  3. ^ "Defence: Drones on Test". 2012-11-03 at the Wayback Machine Flight International, 31 August 1967, Volume 92, Number 3051. p. 350.
  4. ^ "Turkey - Major Army Equipment". from the original on 2 December 2013. Retrieved 27 November 2013.
  5. ^ Taylor 1982, pp. 671–672.

canadair, surveillance, drone, produced, jointly, canada, britain, west, germany, 1960s, larger, improved, model, with, greater, payload, later, introduced, german, army, role, surveillance, drone, national, origin, canada, manufacturer, canadair, first, fligh. The Canadair CL 89 is a surveillance drone UAV produced jointly by Canada Britain and West Germany in the 1960s A larger and improved model with a greater payload the CL 289 was later introduced CL 89 A German Army CL 289 Role Surveillance drone National origin Canada Manufacturer Canadair First flight March 1964 Contents 1 History 1 1 CL 89 1 2 CL 289 2 Description 3 Operators 4 Specifications 5 See also 6 ReferencesHistory editCL 89 edit nbsp Cl 89 NATO AN USD 501 In June 1963 a sponsorship by Canada and Britain 1 2 agreed to have Canadair design evaluate and test the CL 89 drone The concept had been developed at Canadair from the CL 85 a study for the carriage of dispatches West Germany later joined the group 3 and although the United States was invited to join they declined citation needed The first less than successful flight was made at Yuma Arizona in March 1964 The British wanted changes in the system consisting of the drone the launcher the retrieval equipment and the support to be Soldier Proof They sent an army officer to Canadair and with his help set up a maintenance advisory group which had excellent results CL 89 had a difficult development and was almost abandoned citation needed The first complete CL 89 system was supplied to the West Germans in 1969 During the 1970s Both France and Italy joined the British and West Germans in operating the CL 89 NATO gave the entire system the designation AN USD 501 Army Navy Unmanned Surveillance Drone type 501 in UK service it was known as the Midge Military Intelligence amp Data Gathering Equipment The system was designed for information collecting at a divisional level In Royal Artillery service Midge was operated by a troop in a divisional locating battery This troop had two launchers all the facilities for processing and analysing imagery and for repair and servicing of the aircraft The troop comprised two officers and about 70 soldiers Tasking was through the artillery intelligence cell at divisional HQ and the primary use was to confirm suspected enemy locations particularly hostile artillery In UK service Midge replaced the Northrop Radioplane SD 1 known in service as Observer and was replaced in turn by Phoenix Midge was used operationally in Kuwait in 1991 with some effect especially when combined with artillery raids In German Army service CL 89 was operated by a battery in the divisional observation battalion The organisation was similar to the British but had six officers and about 120 soldiers Logistic support for CL 89 was provided to user nations through NAMSA CL 289 edit nbsp CL 289 NATO AN USD 502 In November 1987 an agreement was signed between Canada West Germany and France for the production of the CL 289 system The design of this was started in 1974 It was a larger drone with better range and payload than the CL 89 It was intended to obtain corps level intelligence for the armies of NATO Although similar in appearance to the CL 89 many changes in design were necessary The CL 289 entered service in November 1990 the entire system being designated AN USD 502 At least 9 CL 289 were shot down by the Yugoslavian National Army during the NATO aggression on Yugoslavia in 1999 Description editThe cylindrical body had four stub wings at the rear of the fuselage with aerodynamic trim provided by smaller canard foreplanes Although the drone looked and flew like a missile and was launched from truck mounted rails it cruised under jet power Takeoff was achieved by a booster rocket which was jettisoned when flight speed was attained A small turbojet then took over for the rest of the flightThe flight pattern was programmed and allowed for the flight to the target areas a run while the cameras or sensors recorded and the return to the recovery site On arrival at this calculated position the motor cut and a drogue parachute was deployed This slowed the drone down sufficiently to alter its attitude and allow a parachute to be released from the underside of the drone causing it to invert Before reaching the ground a pair of pneumatic landing bags were released from the top of the drone now facing the ground The retrieval crew would then remove the cameras etc and return the drone to be ready for its next flight A camera or sensor dependent on the mission could be fitted to the CL 89 and multiple units to the CL 289 Being a drone meant that it flew a programmed course and was not under any form of external control In the CL 89 the programmed flight path was constrained by the very limited number of events that could be programmed These events including turns changes in altitude sensor activations de activations and landing The programmed flightpath had to be corrected for meteorological conditions Data for this was provided by a standard artillery Target Acquisition meteor message Two types of sensors were used with the CL 89 both using photographic film that was processed and analysed after the drone was recovered Standard black and white film was normally used in daylight with flares available for night use Infrared linescan an early form of thermal imaging was generally used at night Three types of sensors were used with the British Drone Troops Vinten day sensor Zeiss day and night and IRLS day and night Operators edit nbsp Canada nbsp France nbsp Germany German Army replaced by Rheinmetall KZO nbsp Italy nbsp Turkey Turkish Army 4 nbsp United Kingdom British ArmySpecifications editData from Jane s All the World s Aircraft 1982 83 5 General characteristicsLength 12 ft 2 in 3 71 m with booster Wingspan 3 ft 1 in 0 94 m Diameter 1 ft 1 in 0 33 m body diameter Empty weight 172 4 lb 78 kg Max takeoff weight 343 lb 156 kg with booster Powerplant 1 Williams International WR2 6 turbojet 125 lbf 0 56 kN thrust Powerplant 1 BAJ Vickers Wagtail rocket booster 5 000 lbf 22 kN thrust Performance Maximum speed 460 mph 740 km h 400 kn Range 37 mi 60 km 32 nmi Service ceiling 10 000 ft 3 000 m See also editRelated lists List of missilesReferences edit Defence Archived 2012 11 03 at the Wayback Machine Flight International 29 April 1965 Volume 87 No 2929 p 683 Missiles and Spaceflight Canadair Cl 89 Archived 2012 11 03 at the Wayback Machine Flight International 25 June 1964 Volume 85 Number 2885 p 1082 Defence Drones on Test Archived 2012 11 03 at the Wayback Machine Flight International 31 August 1967 Volume 92 Number 3051 p 350 Turkey Major Army Equipment Archived from the original on 2 December 2013 Retrieved 27 November 2013 Taylor 1982 pp 671 672 Personal experience in Canadair Design Office 1952 75 Picker amp Milberry Canadair The First 50 Years CANAV ISBN 0 921022 07 7 Taylor John W R Jane s All The World s Aircraft 1982 83 London Jane s Yearbooks 1982 ISBN 0 7106 0748 2 Retrieved from https en wikipedia org w index php title Canadair CL 89 amp oldid 1211767873, wikipedia, wiki, book, books, library,

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