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{{Use Canadian English|date=November 2021}}
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{{Use dmy dates|date=November 2021}}
{|{{Infobox Aircraft Begin
{|{{Infobox Aircraft Begin
|name = CL-89
|name = CL-89
|image =Image:CL289_uav_start.jpg
|image = File:CL289_uav_start.jpg
|caption = A [[German Army]] CL-289
|caption = A [[German Army]] CL-289
}}{{Infobox Aircraft Type
}}{{Infobox Aircraft Type
|type = Surveillance drone
|type = Surveillance drone
|manufacturer = [[Canadair]]
|manufacturer = [[Canadair]]
|national origin - Canada
|national origin = Canada
|designer =
|first flight = March [[1964 in aviation|1964]]
|first flight = March [[1964 in aviation|1964]]
|introduced =
|introduced =
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|produced =
|produced =
|number built =
|number built =
|unit cost =
|variants with their own articles =
|variants with their own articles =
}}
}}
|}
|}

The '''Canadair CL-89''' is a surveillance drone ([[Unmanned aerial vehicle|UAV]]) produced jointly by Canada, Britain and West Germany in the 1960s. It was later redesigned and improved, and redesignated the '''CL-289'''.
The '''Canadair CL-89''' is a surveillance drone ([[Unmanned aerial vehicle|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.


==History==
==History==

===CL-89===
===CL-89===
[[File:Cl-89 NATO AN USD-501.jpg|thumb|Cl-89 NATO AN USD-501]]
In June 1963, a sponsorship by Canada and Britain<ref>http://www.flightglobal.com/pdfarchive/view/1965/1965%20-%201239.html</ref><ref>http://www.flightglobal.com/pdfarchive/view/1964/1964%20-%201961.html</ref> 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<ref>http://www.flightglobal.com/pdfarchive/view/1967/1967%20-%201758.html</ref>, and although the USA was invited to join, they declined.


In June 1963, a sponsorship by Canada and Britain<ref>[http://www.flightglobal.com/pdfarchive/view/1965/1965%20-%201239.html "Defence".] {{Webarchive|url=https://web.archive.org/web/20121103054851/http://www.flightglobal.com/pdfarchive/view/1965/1965%20-%201239.html |date=2012-11-03 }} ''Flight International'', 29 April 1965, Volume 87, No. 2929. p. 683.</ref><ref>[http://www.flightglobal.com/pdfarchive/view/1964/1964%20-%201961.html "Missiles and Spaceflight: Canadair Cl-89".] {{Webarchive|url=https://web.archive.org/web/20121103054938/http://www.flightglobal.com/pdfarchive/view/1964/1964%20-%201961.html |date=2012-11-03 }} ''Flight International'', 25 June 1964, Volume 85, Number 2885. p. 1082.</ref> 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,<ref>[http://www.flightglobal.com/pdfarchive/view/1967/1967%20-%201758.html "Defence: Drones on Test".] {{Webarchive|url=https://web.archive.org/web/20121103055019/http://www.flightglobal.com/pdfarchive/view/1967/1967%20-%201758.html |date=2012-11-03 }} ''Flight International'', 31 August 1967, Volume 92, Number 3051. p. 350.</ref> and although the United States was invited to join, they declined.{{cn|date=June 2020}}
The first, less than successful flight was made at [[Yuma Proving Ground|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.{{Fact|date=July 2007}}


The first, less than successful flight was made at [[Yuma Proving Ground|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|date=July 2007}}
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 system the designation AN/USD-501; in UK service it was known as "Midge". The system was designed for information collecting at a divisional level.


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 2 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 [[MQM-57 Falconer|MQM-57]] (SD-1) and was replaced in turn by [[BAE Systems Phoenix|Phoenix]]. Midge was used operationally in Kuwait in 1991.


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 [[MQM-57 Falconer|Northrop Radioplane SD-1]], known in service as "Observer", and was replaced in turn by [[BAE Systems Phoenix|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 6 officers and about 120 soldiers.

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


===CL-289===
===CL-289===
[[File:Canadair CL-89, Friedrichshafen (1X7A4079).jpg|thumb|CL-289 NATO AN USD 502]]
<!-- Deleted image removed: [[Image:CL-289.jpg|right|thumb]] -->
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 and was designated 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 ==
== Description ==
The cylindrical body had four stub-wings at the rear of the fuselage, with aerodynamic trim provided by smaller [[canard (aeronautics)|canard]] foreplanes.
Although both drones had the appearance of missiles, they flew like aircraft and were launched from 'rails' on trucks. They had four large surfaces at the rear of the fuselage with balance control provided by small stabilizers in the nose. Take-off 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

Although the drone looked and flew like a missile and was launched from truck-mounted rails, it cruised under [[jet engine|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 allowing 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.
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 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.
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 [[STANAG 4140|Target Acquisition]] meteor message.


Two types of sensors were used with 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. Infra-red linescan, an early form of thermal imaging was generally used at night.
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==
==Operators==
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* [[German Army]] (replaced by [[Rheinmetall KZO]])
* [[German Army]] (replaced by [[Rheinmetall KZO]])
; {{ITA}}
; {{ITA}}
; {{TUR}}
* [[Turkish Army]]<ref>{{Cite web |url=http://www.globalsecurity.org/military/world/europe/tu-army-equipment.htm |title=Turkey - Major Army Equipment |access-date=2013-11-27 |archive-url=https://web.archive.org/web/20131202230511/http://www.globalsecurity.org/military/world/europe/tu-army-equipment.htm |archive-date=2013-12-02 |url-status=live }}</ref>
; {{UK}}
; {{UK}}
* [[British Army]]
* [[British Army]]
Line 62: Line 69:


{{Aircraft specs
{{Aircraft specs
|ref=Jane's All the World's Aircraft 1982-83 <ref name="Janes 82 p671-2"> Taylor 1982, pp. 671–672.</ref>
|ref=Jane's All the World's Aircraft 1982-83 <ref name="Janes 82 p671-2">Taylor 1982, pp. 671–672.</ref>
|prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
|prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
<!--
General characteristics
General characteristics (CL-89)
-->
-->
|genhide=
|genhide=
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-->
-->
|eng1 number=1
|eng1 number=1
|eng1 name=Williams International WR2-6
|eng1 name=[[Williams International]] WR2-6
|eng1 type=[[turbojet]]
|eng1 type=[[turbojet]]
|eng1 kw=<!-- prop engines -->
|eng1 kw=<!-- prop engines -->
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|minimum control speed note=
|minimum control speed note=
|range km=
|range km=
|range miles=87
|range miles=37
|range nmi=
|range nmi=
|range note=
|range note=
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|more performance=
|more performance=



|avionics=
|avionics=
}}
}}

== References ==
{{reflist}}

* Personal experience in Canadair Design Office 1952-75
* Picker & Milberry, ''Canadair - The First 50 Years'', CANAV ISBN 0-921022-07-7
* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1982-83''. London: Jane's Yearbooks, 1982. ISBN 0-7106-0748-2.


==See also==
==See also==
Line 228: Line 227:
* [[List of missiles]]
* [[List of missiles]]
}}
}}

== References ==
{{reflist}}

* Personal experience in Canadair Design Office 1952–75
* Picker & Milberry, ''Canadair - The First 50 Years'', CANAV {{ISBN|0-921022-07-7}}
* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1982–83''. London: Jane's Yearbooks, 1982. {{ISBN|0-7106-0748-2}}.


{{Canadair}}
{{Canadair}}
{{aviation lists}}


{{DEFAULTSORT:Canadair Cl-89}}
{{DEFAULTSORT:Canadair Cl-89}}
[[Category:UAVs and drones of Canada]]
[[Category:Unmanned aerial vehicles of Canada]]
[[Category:Canadair aircraft|CL-89]]
[[Category:Canadair aircraft|CL-089]]
[[Category:Canadian military aircraft 1960–1969]]
[[Category:1960s Canadian military aircraft]]
[[Category:Military reconnaissance aircraft 1960-1969]]
[[Category:1960s military reconnaissance aircraft]]
[[Category:Single-engined jet aircraft]]

[[Category:Aircraft with auxiliary rocket engines]]
[[ar:كنداير سي إل-89]]
[[Category:Aircraft first flown in 1964]]
[[fr:Canadair CL-89]]
[[Category:Cruciform-wing aircraft]]
[[it:Canadair CL-89]]
[[pl:Canadair CL-89]]
[[ru:CL-89 (БПЛА)]]

Revision as of 09:54, 4 March 2024

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

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.

History

CL-89

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

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

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

 Canada
 France
 Germany
 Italy
 Turkey
 United Kingdom

Specifications

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

Related lists

References

  1. ^ "Defence". Archived 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". Archived 2012-11-03 at the Wayback Machine Flight International, 25 June 1964, Volume 85, Number 2885. p. 1082.
  3. ^ "Defence: Drones on Test". Archived 2012-11-03 at the Wayback Machine Flight International, 31 August 1967, Volume 92, Number 3051. p. 350.
  4. ^ "Turkey - Major Army Equipment". Archived from the original on 2 December 2013. Retrieved 27 November 2013.
  5. ^ Taylor 1982, pp. 671–672.