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{{Use Canadian English|date=November 2021}}
{{Use dmy dates|date=November 2021}}
{{Infobox aircraft
  |name = CL-89
  |image = File:CL289_uav_start.jpg
  |caption = A [[German Army]] CL-289
  |type = Surveillance drone
  |manufacturer = [[Canadair]]
  |national_origin = Canada
  |first_flight = March [[1964 in aviation|1964]]
  |introduction = 
  |retired =
  |status =
  |primary_user = 
  |more_users = 
  |produced = 
  |number_built = 
  |variants = 
}}

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==

===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 "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.{{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 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 [[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 six officers and about 120 soldiers.

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

===CL-289===
[[File:Canadair CL-89, Friedrichshafen (1X7A4079).jpg|thumb|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 [[Armed Forces of Serbia and Montenegro|Yugoslav Army]] during the [[NATO bombing of Yugoslavia]] in 1999.<ref>{{Cite report |last=Lambeth |first=Benjamin S. |year=2001 |title=NATO's Air War for Kosovo: A Strategic and Operational Assessment |url=https://www.rand.org/pubs/monograph_reports/MR1365.html |location=Santa Monica, CA |publisher=RAND Corporation |isbn=0-8330-3050-7 |access-date=14 May 2016 |archive-date=24 March 2022 |archive-url=https://web.archive.org/web/20220324095245/https://www.rand.org/pubs/monograph_reports/MR1365.html |url-status=live }}</ref>{{rp|97}}

== 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 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 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 [[STANAG 4140|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==
; {{CAN}}
; {{FRA}}
; {{GER}}
* [[German Army]] (replaced by [[Rheinmetall KZO]])
; {{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}}
* [[British Army]]

==Specifications ==

{{Aircraft specs
|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 -->
<!--
        General characteristics (CL-89)
-->
|genhide=

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|length ft=12
|length in=2
|length note=(with booster)
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|dia ft=1<!-- airships etc -->
|dia in=1<!-- airships etc -->
|dia note=(body diameter)
|width m=<!-- if applicable -->
|width ft=<!-- if applicable -->
|width in=<!-- if applicable -->
|width note=
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|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
|swept area note=
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|volume note=
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|airfoil=
|empty weight kg=
|empty weight lb=172.4
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=343
|max takeoff weight note=(with booster)
|fuel capacity=
|lift kg=<!-- lighter-than-air -->
|lift lb=<!-- lighter-than-air -->
|lift note=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Williams International]] WR2-6
|eng1 type=[[turbojet]]
|eng1 kw=<!-- prop engines -->
|eng1 hp=<!-- prop engines -->
|eng1 shp=<!-- prop engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=125<!-- jet/rocket engines -->
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->

|eng2 number=1
|eng2 name=BAJ Vickers Wagtail
|eng2 type=rocket booster
|eng2 kw=<!-- prop engines -->
|eng2 hp=<!-- prop engines -->
|eng2 kn=<!-- jet/rocket engines -->
|eng2 lbf=5000<!-- jet/rocket engines -->
|eng2 note=
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|eng2 lbf-ab=<!-- afterburners -->

|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=<!-- prop engines -->
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|eng3 lbf-ab=<!-- afterburners -->
|more power=

<!--
        Performance
-->
|perfhide=

|max speed kmh=
|max speed mph=460
|max speed kts=
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=<!-- aerobatic -->
|stall speed mph=<!-- aerobatic -->
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
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|range km=
|range miles=37
|range nmi=
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|combat range km=
|combat range miles=
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|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=10000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
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|time to altitude=
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|more performance=

|avionics=
}}

==See also==
{{Portal|Electronics|Aviation}}
*{{anl|Joint Electronics Type Designation System}}
*[[List of military electronics of the United States]]
* [[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}}

{{DEFAULTSORT:Canadair Cl-89}}
[[Category:Unmanned aerial vehicles of Canada]]
[[Category:Canadair aircraft|CL-089]]
[[Category:1960s Canadian military reconnaissance aircraft]]
[[Category:Single-engined jet aircraft]]
[[Category:Aircraft with auxiliary rocket engines]]
[[Category:Aircraft first flown in 1964]]
[[Category:Cruciform-wing aircraft]]
[[Category:Canard aircraft]]

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