Showing posts sorted by relevance for query ababil. Sort by date Show all posts
Showing posts sorted by relevance for query ababil. Sort by date Show all posts

Saturday, February 5, 2011

Ababil UAV

Index

Introduction
Acronyms and Abbreviations
Executive Summary
Ababil-1

- Development 
- Technical Assessment 
- Use 
Ababil-2 
- Development 
- Technical Assessment 
- Specifications 
- Variants
- Use 
Ababil-3 
- Development 
- Technical Assessment 
- Use 
- Recognition Features 
Other 'Ababils' 
Appendix: Documented Airframes / Serials 
Footnotes / Works-Cited

HESA's booth at the 2012 Kish Airshow


Acronyms and Abbreviations

Executive Summary:

  • Production & Development 
    • Developed and produced by HESA. This is in contrast to most Iranian UAVs, which are developed by the Qods Company. Both Qods and HESA are subsidiaries of the MODAFL-owned Aviation Industries Organization.
    •  Total production reportedly ~370 by 2006, with a production rate of ~70/year.
  • Technical Characteristics and Variants
    • All variants are classified as tactical UAVs with a range of 100+ km, a ceiling of ~4,000 m, and an endurance of up to several hours. 
    • Ababil-1 (AB1): Disposable attack drone built during 80s. Assumed to have been phased out of service. 
    • Ababil-2 (AB2): Reusable target-drone with rudimentary surveillance capabilities. Can be used as disposable strike munition. Developed during the 90s, it is characterized by its delta-wing and canard configuration. Up to two hour endurance. 
    • Ababil-3 (AB3): Larger, more capable, and longer ranged surveillance variant developed during the 00s. Similar appearance to, and suspected development from, South Africa's Seeker. 
  • Use in Iran
    • AB2: Widespread use as a target-drone through the present. Surveillance use suspected, but undocumented in practice. Ongoing replacement by the AB3 possible. 
    • AB3: Increasing use in Iran by IRGC and IRIAF from 2010 onward, particularly in maritime environments. 
  • Use Outside Iran
    • AB2: Occasional use by Hezbollah through mid-2000s. May be found elsewhere (e.g. Gaza).
    • AB3: Widespread foreign use; documented rarely in Sudanese government use in late-00s, and frequently in the hands of (pro-)government forces in the Syrian civil-war 2012-present. Possible use by (pro-)government forces in Iraq 2014-present.

Ababil-1 (AB1) 

 Development:
The first variant of the Ababil family was developed by the IEI's mechanical-industries department in the mid-80s. In 1986, the design was transferred to HESA for mass production.1

Technical Assessment:
Design details, or even the AB1's basic configuration, are unknown. Unlike its contemporaries, such as the early Mohajers, the AB1 was designed as a disposable precision-guided munition with a 40 kg warhead.

It is unknown whether or not the AB1 was employed during the war, let alone the details of its tactical employment. The most plausible explanation is that it was employed as a short-range precision munition against Iraqi defenses. It is suspected that a direct hit would create enough overpressure to destroy field-expedient and reinforced fortifications. Against personnel and other soft targets, it would have been less effective due to a lack of fragmentation.

Use:
Unknown

Ababil-2 (AB2)


Development
:
In 1991, HESA embarked on a redesign of the Ababil based on new requirements issued by the the Armed Forces for a reusable UAV. The new design entered production in 1992.2 In 1999, the AB2 was documented publicly for the first time in the UAE's IDEX '99 arms exhibition, where it was offered for export.3 Today, it is marketed by HESA for military surveillance, communication-relay, and civil use.

Technical Assessment
:
Each of the AB2-variants share the following characteristics:
- Cylindrical fuselage
- Cropped-delta wing with ailerons to control roll
- Canards with elevators to control pitch
- Pneumatic or rocket-assisted takeoff / parachute recovery

WAE-342, aka MDS-342 (Meggitt Brochure)
All variants are powered by the 25 hp WAE-342 twin-cylinder piston engine fitted with a pusher prop. Produced by the UK's Meggitt Defense Systems, this model is widely used in other UAVs. In Iran, it is also found on the Saeqeh target drone. It is assessed with low confidence that this engine has been produced since 2010 by the Qom-based MADO Company under the name “MD-275”.4 Although HESA initially advertised the optional installation of the more powerful AR-731 rotary engine (aka the P-73), this has not been documented.5

Range and endurance are primarily limited by the AB2's small 16 liter fuel tank. According to HESA, its endurance is 1 ¼-2 hours and its operational radius is 100 km (with no loiter time).6 7 At this range, the issue of BLOS control is unlikely to be a major issue as HESA states that the maximum range of LOS control is 120 km.

The Ababil can be fitted as needed with electronic subsystems to assist in flight control.8 These include data links for real time telemetry and video transfer, automated controls that remove the need for active pilot control, GPS/INS-cued waypoint navigation, and pre-programmed mission profiles. These features reduce pilot workload, allowing the operators to focus on their mission rather than keeping the UAV airborne. It also means that it can be programed to fly beyond-the-line-of-sight (BLOS). In order to support the data links, two stubby antenna are typically fitted, one each at the front and back of the fuselage.

Variants
:
A handful of sub-variants exist, but there is little consensus over their designations or their characteristics. One of the more detailed descriptions comes from Iran's Mashregh News.9 This agency is reportedly linked to the IRGC, and often publishes articles with a military focus, indicating that their claims are credible.10 However, many of their articles also contain open-source analysis and speculation, making their overall credibility difficult to assess. Other descriptions of specific sub-variants are similarly unsourced, and whose credibility is even harder to assess. 11

Three sub-variants of the AB2 can be confidently identified: a target drone, a surveillance model, and a variant fitted with twin-tails. The first and second share a basic airframe, and it is a reasonable assumption that they are identical apart from the payload. A fourth variant, fitted with an explosive payload, is less well documented.  

Aerial Target:
This frequently documented variant is used for air-defense training, and can be recognized by the lack of a camera. It is typically fitted with a single whip antenna on the nose for receiving flight controls.

Reported payloads include miss-distance-indicators (used for gunnery training), IR beacons (used with MANPADS), and radar reflectors (used with radar-cued systems).  
 
JATO prep for IRIN gunnery training, Blow of Zolfqar exercise, 2006 (FNA)


Surveillance:
Employed for tactical surveillance, this variant is characterized by a) an electro-optical payload, and b) additional flight control equipment described above. Compared to similar surveillance UAVs, both in and out of Iran, the Ababil has only the most rudimentary capabilities, and is hampered by a low endurance and basic payload.

Two payload configurations have been documented. The first is fitted in a conventional gimbal below the fuselage, while the other is fitted in the fuselage's nose, much like the seeker on a TV-guided missile.12 Both configurations are limited to daylight TV cameras due to weight and size limits.

Twin-Tail:
The third variant is characterized by the use of two vertical stabilizers. Although structurally different from the two variants listed above, it can be used in either role when fitted with the respective payloads.

Mashregh News reports that the tail configuration allows for an increase in speed and range due to aerodynamics and antenna location. This cannot be confirmed and may be unlikely given that documented examples show near-identical antenna configurations. They also report that it is built from composites (e.g. fiberglass), which would give it a lower weight, and a lower RCS than its aluminum counterparts. 13

One example seen on parade in Tehran, was designated the “Ababil-CH” and used as a target drone. Another example, used by Hezbollah, was fitted with the nose-mounted camera and a non-standard engine. At least one of Hezbollah's examples has been shown fitted with a non-standard engine.

Disposable Strike Munition:
Little is known about this version, which has only been documented indirectly in conjunction with Hezbollah.

It reportedly carries a 30-50 kg warhead, which is consistent with the AB1's payload described above.14 15 It is unknown whether or not a camera and data-link are fitted, which would allow it to be used for precision-strike. Given a total payload capacity of 40 kg, this would only be feasible with the smaller warhead. A larger payload would be limited by the accuracy of its GPS/INS-pathfinding, and preclude midcourse corrections.

Although this variant is typically associated with the twin-tail airframe, it is a reasonable assumption that its payload can be fitted to the single-tail airframe as well.

Specifications
:
Length: 2.8 m
Wingspan: 3.25 m
Weight, Empty: ~30 kg
Weight: Payload: 40 kg
Weight, MTOW: 83 kg
Speed, Cruise: 250-305 km/h*
Ceiling: ~3,000+ m
Endurance: 1 ¼ – 2 hr

* Different sources report different speeds, both for 'maximum' and 'cruise'. When the AB2 was first unveiled in 1999 with the AR-731 engine, it's maximum speed was quoted at between 340-470 km/h (although the latter was described as its cruise speed). In the early-00s, its cruise speed was listed as 305 km/h with the WAE-342 on HESA's website. However, in the most current MODAFL export catalog, its maximum speed is listed as 250 km/h.

Use
:
Mohammed Rasoollallah exercises, December 2014
In Iran, the AB2 has frequently been documented in use as a target drone by both the IRGC and the Army. The surveillance and twin-tailed examples have only been seen on parade and in HESA booths at trade shows, suggesting that they may not be operationally deployed


Around 2006, 369 Ababils had been reportedly built in total.16 Out of this total, 68 had been built in 2006, of which HESA had originally planned to export 13; 71 had been built the year before, 20 of which were exported.17 18 Although these numbers may include the AB1 or AB3 (which HESA began to acquire around this time), it is assumed the majority correspond refers to the AB2. Of the total number, an unknown quantity were target drones, many of which would have been destroyed in routine service.

In Lebanon, Hezbollah operates the twin-tail variant known locally as the 'Mirsad-1', where it is fitted with surveillance or explosive payloads. They are used strategically for messaging, and gathering intelligence. There are no known instances of tactical surveillance use. In the strike role it may be used tactical or strategically.

The Mirsad/AB2's twin-tails just visible in 2004 flight (al-Manar/NBC)
The first documented case occurred in November 2004 when an Ababil overflew the coastal town of Nahariya 10 km south of the Israel-Lebanon border, spending between five and 20 minutes loitering over the city before returning to Lebanon.19 20 Afterwards, Hassan Nasrallah, Secretary General of Hezbollah, gave a speech where he identified the UAV as a Mirsad-1, and claimed that it could carry a 40-50 kg warhead to strike various strategic targets.21 Nasrallah's speech, and the filmed flight indicates that Hezbollah intentionally used it for its messaging potential.

In April 2005, a surveillance Mirsad flew nearly 30 km south of the border before returning to Lebanon, spending a total of 18 minutes over Israel. Although IAF jets were scrambled, they failed to intercept it.22

Prior to the 2006 33-Day War, the IDF estimated that Hezbollah was in possession of 12 Ababils.23 Others estimated that the number could have been as high as 24-30.24 Both estimates are likely to be no more than educated guesses, but are generally consistent with self-reported production. During the war, at least three were launched.25 The first was shot down by the IAF on August 7 off the coast of Haifa, about 30 km south of the border. Its remains were recovered and photographed. The second was shot down on August 13 about nine km south of the border, near Kibbutz Cabri. This example was reportedly packed with a 30 kg explosive payload. The third was launched the shortly afterward on the same day, but crashed inside Lebanon near the city of Tyre.

No AB2s have documented in use over Syria from 2012 to the present, possibly suggesting that they have been supplanted – in the surveillance role at least – by the latest generation of Ababils. In 08/2012, insurgents captured a government workshop in Aleppo and a handful of rudimentary UAVs that were distinct from, but similar to, a number of Iranian designs including the AB2. Moreover, technical manuals with Khomenei's picture on the cover were also recovered, suggesting that these examples were being built with Iranian assistance.26

In the Gaza Strip, a UAV physically similar to the AB2 was documented in November 2012 when an Israeli surveillance flight captured its taxi test in Khan Yunis.27 The taxi-test indicates that this model had been fitted with conventional landing gear for takeoff and recovery.

Ababil-3 (AB3)


The latest member of the Ababil family is the AB3. Strikingly similar to the South-African Seeker, the AB3 is a far more capable surveillance platform; it can remain airborne longer, and carry a more sophisticated payload. It is increasingly deployed, both in Iran and abroad, for tactical surveillance.
AB3 at Kish Airshow, 2014 (IRNA)


Development:
Details of the AB3s development are unknown, but it is a reasonable assumption that it was reverse-engineered from the Kentron/Denel Seeker.

One possible explanation is that Denel supplied Iran with an unknown number around 2005-2006, which were then either locally assembled, reverse-engineered, or simply re-badged. This is based off a lawsuit filed by a Turkish company in 2012 that alleges MTN, a South-African telecom giant, bribed Tehran with promises of arms sales, including the Seeker, in order to secure a lucrative contract inside Iran.28 However, the filing also described how MTN failed to deliver on these promises over the following years – by which point the AB3 had already been documented. Additionally, one Denel official told Reuters that although they had proposed selling Iran certain UAV-related technologies, the deal had been blocked by the South African government.29

Nonetheless, this possibility should not be dismissed. First, the descriptions of Iranian frustration with MTN's failures focus on attack helicopters, not the other products. Second, Denel's explanation that their ostensibly legal discussions with Iran never amounted to anything lose credibility given parallel – and vehement – denials of ever having any contact with Iran.30

It is assessed with high confidence that specific characteristics of the AB3 indicate it was developed from Seekers fielded during the early-90s.31 32 These include vertical stabilizers with a vertical leading-edges, the absence of flaps on the inner wing's trailing-edge, and the use of Limbach engines. However, certain inconsistencies means that it can only be assessed with moderate confidence that the AB3 is most closely related to the Seeker-2D. This uncertainty might be explained by the fact that the AB3 is locally produced rather than a direct export, or by the somewhat opaque development of the Seeker itself.

The AB3 ostensibly entered production by 2006.33 This short production timeline casts further doubt on, but does not rule out, the MTN connection described above. It was first sighted in 2008 over Sudan, but it was not seen in Iran until 2010. Since 2012, it has been regularly documented in Iran and abroad.

Technical Assessment:
The Seeker origin gives the AB3 a significant step up over earlier Ababil generations. A more powerful engine and a larger fuselage allows it to carry more fuel, fly higher, and carry a wider range of surveillance payloads.

"MD 550" on display, 2014 (Military.ir)
The AB3 is powered by the 50 hp L-550E four-cylinder piston engine fitted with a pusher prop. This engine is also used on Seekers developed during the 90s, and on some of Iran's Mohajer-4s. As late as 2009, engines were illegally procured from Limbach, their German manufacturer, using intermediaries.34 Qom-based MADO now claims to be producing them domestically under the name “MD-550”.35

At least one Seeker variant pairs this same engine with a 64 l (standard) or 79 l (extended range) fuel tank, which gives it a 10 hour endurance. However, this number likely refers to a model which utilizes fuel stores in the wings, a model that postdates the one Iran's AB3 most closely resembles. This would explain the apparent disparity between the 4 hour endurance provided by Mashregh News, and numbers associated with the Seeker.36

Ground control station, 2010 (PressTV)
However, the AB3 is more likely than the AB2 to be limited in range by its LOS control. Although it can fly beyond its nominal 100+ km range, it cannot be actively controlled while doing so. For BLOS control, the the AB3 appears to be fitted with much the same guidance and control capabilities as the AB2, although it's unknown if the actual systems themselves are the same.37

The AB3 can be fitted with up to three different payloads: a) a gimbaled EO-system for surveillance, b) a fixed downward-facing still camera for aerial surveying, and c) a fixed oblique camera in the nose for navigation and takeoff/landing. This contrasts to the AB2's single daylight camera.

The gimbaled system is used for real time surveillance and includes a daylight camera, thermal imager, and laser range finder. The exact model and its specifications are unknown, but appears comparable to the top of the line system offered for export by MODAFL-subsidiary Isfahan Optical Industries (IOI).

Use:
In Iran, the AB3 has been used by the IRGC's Aerospace Force since at least 2010, and by the IRIAF since at least 2013. It was first documented in the IRGC-ASF's Great Prophet 5 exercises in 04/2010. At the same time, Iranian media announced the intended mass production of an unspecified UAV for the IRGC-ASF, which suggests an order had been placed. It was again seen during the IRGC-ASF's Great Prophet 7 exercises in 07/2012. Then, in 12/2013, an AB3 was shown taking off from the IRIAF's airbase at Bandar-e Abbas, where it was participating in their Velayat-4 exercise. Shortly thereafter, in 02/2014, another AB3 was photographed at an open house held at the IRIAF's airbase at Konarak.
IRIAF AB3, Velayat-4, 2013 (IRNA)

The very first AB3 was documented, not in Iran, but in use by Sudanese government in 05/2008. In discussions with UN peacekeeping forces, the local commander confirmed that 3-5 airframes were operating out of the al-Fashir airport in western Sudan.38 39 Associated infrastructure, including a GCS and at least one hanger, were documented in handheld imagery provided to the UN, and in open-source overhead imagery. Witnesses reported sightings in at least two other west-Sudan airports.

In Sudanese service, AB3s – known locally as the Zagil – were used by Khartoum for security operations over South Sudan, before and after their 2011 independence. They were employed for surveillance, and precision targeting. In the latter role, they would take advantage of low airspeed and high endurance to pinpoint targets for higher-flying bombers.40 Foreshadowing the same tactic used only a few years later in Syria, many of these 'bombers', were in fact cargo planes fitted with improvised barrel bombs that would be pushed out the rear hatch.

At least two examples have been shot down by anti-government forces, the first in 08/2008, and the second in 04/2012. The second example carried a badge indicating that it had been manufactured by HESA in 2006. Both examples carried a range non-Iranian components. The first example carried a UK video recorder, and the second carried electrical connectors made by the French company “Souriau FR”, and Irish carburettors. The Souriau components are of particular note since this company was referenced in Wikileak's cables, when Washington tried to advise Berlin of attempts by an Iranian front company to procure components for their UAV program.41
AB3 downed over Sudan in 2012 (Sat Sentinel Project)


It is in Syria, however, that the AB3 has been the most prolific. For detailed documentation of their use through 01/2014, see a report by author at OSIMINT, titled: “UAVs over Syria”.42 Since then, their use has shown no signs of abating.

Examples that have been shot down and recovered by anti-government fights show that they carry both gimbaled sensors for real-time surveillance, and fixed aerial survey cameras. The former would be used for spotting targets and cuing artillery or airstrikes by fixed or rotary-wing aviation. The survey cameras would be used to create up-to-date maps distributed to ground forces during attacks. The use of such maps has been documented widely, but cannot be conclusively linked to the AB3. In all of these roles, the unmanned, low-and-slow-flying AB3 offers a marked advantage over more expensive and less capable manned aircraft. In particular, its thermal imaging payload is unique among the government's stock of aging Soviet hardware.

It is unclear who is operating the AB3s over Syria. The most likely candidates include the IRGC themselves, the Syrian Air Force, or Hezbollah. Similarly, it is unknown which airports they operate out of.

In Iraq, the AB3 may be in use by pro-government forces, but this has yet to be confirmed.43

Other 'Ababils' 

Beyond the AB1, 2, and 3 described above, there are a handful of projects that may or may not be tangentially related to this family.

Sub-scale aircraft that superficially resemble the AB2 are sometimes seen in HESA booths at trade shows (see first photo from Kish 2012). It is suspected that these are student projects, which are indirectly affiliated with HESA.44

In 2009, an article by UAS Research indicated that there were two more Ababil variants in development.45 The first was a hand-launched version, and the second was a jet-powered version named the “Hadaf-1”, fitted with the Touloue-4 engine also used on Iran's longer-ranged ASCMs. No details about the hand-launched version was provided, and there has been no indication since then to indicate its existence.

It is confidently assessed that the 'Ababil Jet' – also known as the Hadaf-1 – is a reference to what is now known as the Karrar, which was publicly unveiled in 2010. The name 'Hadaf', which means 'target', suggests that it was intended as a replacement for Iran's US-supplied MQM-107 target drones, which is consistent with the Karrar's documented employment thusfar. The project was first documented in 2002 when HESA's vice-president noted that the company was already marketing an unnamed jet-powered craft in the same class as the MQM-107 and the Karrar. 46 The VP's article was accompanied by a picture from the HESA labs showing a jet-powered mockup that was nearly identical to the Karrar's final design. A model of this design was also shown to Ali Shamkhani when he was still Minister of Defense, around 2004.

Appendix: Documented Serials
(to be updated)
AB3, Iran
:
2-2-S012 (?)
2-2-S043
2-2-S134
2-2-S162
2-2-S164
2-2-S176
2-2-X31
2-2-S203
X-X-X259

AB3, Sudan:
3-1-R031 (Downed in action, aka Zagil, built 2006)

AB3, Iran:
3-1-R023 (Early development example, suspected)
3-2-R050 (IRGC Exercise, 2010)
X-X-R124 (Display during Rouhani's 08/2014 visit to defense show)
3-2-R126 (Display during Nigerian government visit)
3-2-R155 (Display, Kish Airshow, 2014)
6-2307 (IRIAF Exercise, 2013)

AB3, Syria:
3-2-RXXXX (05/23/13)
3-2-R-0105 (06/12/13)
3-2-R-010X (10/08/13)
X-X-R-1003 (12/19/13)
X-X-R-2004 (?) (10/02/13)

Footnotes / Works Cited
1) Iran's Ababil … [unclear]. Mashregh News. 10/11/11 
2) ibid Mashregh News, 10/11/11
3) Iran Tests Unmanned Air Vehicle. Flight Global. 04/28/99
4) Self Sufficiency in the Production of UAV Motors / Iranian Researchers Successfully Built UAV Motors. ISNA. 07/27/2010.
5) HESA product advertisement. Website now defunct, but entry reproduced by the ACIG Forums 02/2004.
6) HESA product advertisement. Website now defunct, but entry reproduced by the ACIG Forums 02/2004.
7) Ababil 2 UAV System. MINDEX.
8) ibid Mashregh News, 10/11/11
9) ibid Mashregh News, 10/11/11
10) The specifics of its links to the IRGC are unknown. For an example of such a claim, see link.
11) Ababil (Swallow) Unmanned Air Vehicle. Global Security.
12) One exception to this is an example paraded in Tehran in 09/2008, which featured the sensor gimbal above the fuselage. One explanation is that the payload module was accidentally installed upside down for the parade.
13) This cannot be confirmed, but a handful of images show the single-tailed Ababils assembled with riveted panels, which is typically associated with aluminum rather than composite construction, which can be bonded together with less mechanical fasteners.
14) Hezbollah Drone Threatens Israel. NBC Nightly News. 04/12/05
15) Hezbollah drone brought down over Galilee held 30 kg of explosives. Haaretz. 08/14/06.
16) Unidentified defense-industry show open to the public. Data was presented on a poster, which was photographed and uploaded to military.ir and iranmilitaryforum.net.
17) ibid defense-industry poster.
18) HESA to Enhance Nation's Fleet by 71 More Birds. Mehr News. 01/23/2006. Original article inaccessible, but article reproduced on ACIG Forums, 01/2006.
19) Air force: Hezbollah drone flew over Israel for five minutes. Haaretz. 11/09/04
20) ibid NBC Nightly News, 2005
21) ibid NBC Nightly News, 2005
22) Air Operations in Israel's War Against Hezbollah. Benjamin s. Lambeth. RAND. 2011. p.131
23) ibid Lambeth, 2011
24) Preliminary “Lessons” of the Israeli-Hezbollah War. Anthony Cordesman. CSIS. 08/17/06. p.5
25) ibid Haaretz, 08/14/06
26) Syrian regime's drone workshop with Saeqeh UAVs (and evidence of Iranian support) captured by the rebels in Aleppo. The Aviationist. 08/12/12
27) Hamas Test Running a UAV in Khan Yunis, Gaza. Idfnadesk. Youtube. 11/16/12
28) Case 1:12-cv-00479-RBW. Document 1. Filed 03/28/12. p.50
29) MTN and Iran 'No Normal Country'. Steve Stecklo w and David Dolan. Reuters Special Report. 06/25/12.
30) Private correspondence between author and Denel, 2011
31) 10 Squadron, AFB Pochefstroom - Seeker UAV. SAAF Forum.
32) Seeker 1. Unofficial Website of the South African Air Force.
33) Based on DOMs on an example recovered in Sudan in 2012.
34) Germany tries Iranians charged with smuggling drone engines as jet ski parts. Reuters. 06/16/14.
35) Imagery from trade show in October 2014 and elsewhere shows these engines offered for export, and in various states of assembly.
36) Iran's Newest Ababil Ready to Attack … [Unclear]. Mashregh News. 06/30/14
37) Ababil 3 UAV System. MiNDEX http://www.mindexcenter.ir/product/ababil-3-uav-system
38) Security Council Committee report, S/2009/562. Link
39) Security Council Committee report, S/2008/647 Link
40) Sudan Armed Forces Implicated in Video Captured by Their Own Drone. Jonathan Hutson. Satellite Sentinel Project. 04/10/1
41) UAE-Based Front Company for Iranian Procurement Entity Seeks French-Origin Connectors from German Firm(s). 01/09/09. Wikileaks.
42) UAVs Over Syria. OSIMINT. 01/08/2014.
43) Iran Secretly Sending Drones and Supplies Into Iraq, U.S. Officials Say. NYT. 06/25/14
44) HESA hosts a festival, possibly yearly, for student designs and RC-flight enthusiasts at their facility near Isfahan. Pictures from the event include the wheeled 'Ababil' in question.
45) 2009/2010 UAS Yearbook. 7th Ed. Blyenburgh & Co, 2009 46) Iran Joins the Aircraft Industry. Iran International. 10/01/02

Thursday, March 5, 2015

Mohajer UAV

Index:
Introduction
Mohajer-1
- Development
- Technical Assessment
- Use
- Recognition Features
Mohajer-2
- Development
- Technical Assessment and Specifications
- Variants
- Use
- Recognition Features
Mohajer-3
- Development
- Technical Assessment and Specifications
- Use
- Recognition Features
Mohajer-4
- Development
- Technical Assessment and Specifications
- Variants
- Use
- Recognition Features
Appendix: Documented Airframes and Serials
Footnotes/ Works-Cited

Introduction:

The Mohajer family encompasses a range of tactical surveillance UAVs, and are among the most well known and mature Iranian designs. Developed during the height of the Iran-Iraq war by the Qods Aviation Industry Company, they continue to be used by various branches of the Iranian military. Though not as widespread in foreign service as the Ababil, they have increasingly been seen over Iraq and Syria.

The Mohajer's name is often translated as immigrant or emmigrant, but is likely intended to specifically invoke the Arabic muhajirun and muhajir, which – respectively – refer to Mohammed's original 'emmigration' to Mecca, and those that have made the pilgrimage since.

Mohajer-1 (M1):

Fielded under wartime pressures, the Mohajer-1 was a relatively unsophisticated design. Although it had only a minor impact on the overall course of the Iran-Iraq War, the tactical experience helped lay the institutional foundations for Iran's development and use of unmanned aircraft over the following decades.

Development:
The Mohajer-1 was developed following the IRGC's first forays into unmanned reconnaissance in the early-1980s. By 1985, the Qods Industries was formed as a wing of the IRGC's self-sufficiency department and tasked with supplying the nascent Raad Brigade. The M1 was developed sometime that same year.

Technical Assessment:
(Soureh Cinema)
An impediment to assessing the M1 is the lack of documentation. Much of the imagery purporting to show wartime M1s are from “Mohajer”, a movie released in 1990. 1 2 However, given the government's role in making war movies, it is a reasonable assumption that the portrayal is fairly accurate.

Physically, the Mohajer-1 is characterized by a narrow cylindrical fuselage, twin-boom tails, and straight wings high and to the rear of the fuselage. It is similar in size to the RQ-7. For flight control, the M1 is fitted with an elevator on the horizontal stabilizer to control pitch, rudders on the vertical stabilizers to control yaw, and ailerons on the wings to control roll.

A tricycle landing gear is employed for launch and recovery. A parachute can also be used for recovery.

(Soureh Cinema)
For surveillance, the M1 is fitted with a single oblique camera in the nose. Based on other Iranian UAVs from this period, it is likely that this was a still camera, whose film was processed after recovery. One source indicates that it could transfer real-time imagery, though this is questionable. 3

The Mohajer-1 could also be armed and the 1990 movie shows it fitted with 3-round RPG launchers under each wing.

The M1 is controlled via hobby-class radio-control (under 100 mhz). 4

Use:
During the Iran-Iraq War, the IRGC's Raad Brigade operated an unknown number over the southern front. Although the they first used UAVs during Operation Kheibar (Feb/March 1984), and Badr (March 1985), the Mohajer in particular is first associated with Operation Valfajr-8 (Feb 1986), and Karbala-5 (Jan/Feb 1987). 5 They were used to prepare for these offensives by photographing Iraqi positions. 6 They were also reportedly used for artillery correction, but it is unclear if this took place in real time, or were used for assessment after the fact.

In the 1990 movie, two teams of personnel are shown: a rear-area launch section, and a forward control section. The need to forward deploy the operators was the result of the radio-control, which limited signal power and precluded data transfer. This, in turn, meant that the M1 could only be used over the front line, and lacked the ability to reconnoiter in depth.

There are reports of Iraqi forces jamming Iranian UAVs by using their HF/VHF/UHF radios, which would have operated in a similar frequency. 7

There are no reports of how effective the M1's armament was. However, given the manual line of sight control, it is unlikely to have been too accurate. This is one area where the movie takes artistic license, purporting to show real time targeting via the on-board camera. In addition, some report that this armament was tested as an anti-shipping weapon in the Gulf. 8
Spotting artillery impacts during Karbala-5 (UAS Yearbook)


Mohajer-2 (M2):

The Mojajer-2 is representative of the intermediary generation of Iranian UAVs developed during the 90s. In this regard it is largely equivalenent to the Ababil-2, both in generation and in capabilities (e.g. MTOW, endurance). However, unlike the Ababil, the M2 is still routinely used for ISR. Although its capabilities are downright modest compared to the current generation designs, updates promise to keep the M2 relevant.
NEZAJA M2 during Mohammed Rasoolallah Exercises, December 2014 (Jam-e Jam)


Development:
1996 parade (Getty)
The Mohajer-2 was developed prior to 1996, when it was documented on parade in Tehran. Then, in 1999, the Qods company announced that they would host a flight demonstration alongside the Mohajer 3 and 4 (though there is no record of said demonstration). 9 The M2 was next documented during the 2005 Kish Airshow. 10 Since then, the M2 and its variants have been documented regularly.

As of the mid-2000s, 253 Mohajers had been produced. Although it is impossible to say how many of these were M2s, it is a reasonable assumption that they comprised the bulk of this number.

In 11/2014, a new generation was unveiled at that year's Kish Airshow, boasting greatly improved performance.

Technical Assessment:
Physically, the Mohajer-2's airframe is an evolution of the Mohajer-1 design. It is characterized by the same cylindrical fuselage, twin-boom tails, and straight wings. Its flight controls are the same, including an elevator on the horizontal stabilizer, rudders on the vertical stabilizers, and ailerons on the wings. Subtle variations in M2s, such as the engine nascalles, indicate slight changes in manufacturing over time.

The use of skids, rather than the M1's tricycle gear, means that the M2 is dependent on pneumatic or rocket assisted launch (usually the former). Recovery is by parachute or conventional landing.

The Mohajer-2 is powered by the 26 hp WAE-342 twin-cylinder piston engine fitted with a pusher prop, which is also used on Iran's AB2 and Saeqeh. However, a handful of examples have atypical exhaust systems, possibly explaining the discontinuity between the 342's known power, and the 25 hp consistently claimed on M2 brochures. Official advertisements claim an operational range of 50 km (100 km ferry range), and an endurance of 1.5 hours.

The M2 is fitted with two stub antenna, one on either wing. These support the higher frequency datalinks that allow for real-time control (under 10 ghz).Like the Ababil family, the lack of OTOH control is unlikely to be a significant problem given its short range. Although exact details are scant, export brochures indicate that it is fitted with control software that allows the Mohajer to be flown in one of three modes: manual, semi-automatic, and automatic.

- Manual: The operator controls all aspects of UAV flight by using the real-time feed from the onboard cameras. This mode relies on high and low bandwidth communication between the UAV and GCS.
- Semi-automatic: The operator determines the UAV's flight path, but does not control the flight itself. This mode relies on the lower bandwidth control and telemetry channels, which have a longer range than the higher frequency channels used for imagery downlinks.
- Automatic: The UAV follows a preset flight path and executes commands using GPS and INS-cued waypoints. This mode does not require any uplink/downlink between the UAV and the GCS.

NEZAJA display, 2009 (Unknown)
Forward-facing and gimbaled cameras
The Mohajer-2 can be fitted with three different optical payloads: a) a gimbaled EO-system for surveillance, b) a fixed downward-facing still camera for aerial surveying, and c) a fixed forward-facing camera in the nose for flight. The gimbaled imager is used for real-time surveillance and is limited to light-weight models by the M2's relatively small payload. In practice, only daylight cameras, such as the IEI's Oghab 11, have been fitted. Early-production M2s lacked the forward-facing camera.

Product brochures also advertise the use of laser line scanners (for wide area aerial surveying), and unspecified electronic-warfare payloads. Neither of these have been documented.

Like the M1, the M2 can also be armed. Documentary footage shows development models fitted with two six-round RPG launchers. However, these have not been documented in service.

Specifications (M2):
Length: 2.91 m
Wingspan: 3.8 m
Weight, Empty: 70 kg
Weight: Payload: 15 kg
Weight, MTOW: 85 kg
Speed, Max: 200 km/h
Ceiling: 3,350 m (11,000 ft)
Range: 50 km
Endurance: 1.5 hours
Powerplant: 25 hp L-275

Specifications (M2N):
Length: 2.90 m
Wingspan: 3.82 m
Weight, MTOW: 90 kg
Speed, Max: 180 km/h
Range: 150 km
Endurance: 6 hours

Variants:

Raad-85:
It is assessed with low to moderate confidence that the Raad-85 is a 'suicide' strike variant of the M2, comparable to the similarly equipped Ababil-2 variant. Its designation may be associated with the NEZAJA in particular.

The first reference to the Raad came in 02/2011 when then-DM Vahidi announced the manufacture of an offensive UAV capable of precision strike. 11 Then, in 10/2011, Mashregh News described the Raad as a variant of the Saeqeh target drone (also produced by the Qods Company). 12 Although there was no reason given for this claim, and at first glance appears to be a product of their own open-source research, this possibility cannot be dismissed. The most significant evidence for the Raad's link to the M2 came during the IRGC's Great Prophet 8 exercises in 02/2013, which showed unnamed M2-based UAV being used in the suicide strike role.
Suicide M2 being prepared for launch during 2013 exercise (IRIB)


Finally, during a delivery ceremony in September 2013, the NEZAJA announced that they were producing the Raad-85 in cooperation with the Qods Company. 13 At the ceremony, both the M2 and Saeqeh were on display, providing no further clarification.

Specifications for the Raad are elusive. In 09/2013, a NEZAJA commander claimed the Raad had a 100 km range (equivalent to the M2). 14 Then, during a later exercise in 12/2014, another commander said that the Raad had a range of 250 km, suggesting a closer relationship to the M2N than the much shorter ranged M2 or Saeqeh. 15 16

Mohajer-2N:
The M2N (the 'N' stands for 'new') was unveiled during the 2014 Kish Airshow. Nearly identical to the M2 in outward appearance, it reportedly enjoys a significant increase in performance. This includes a 200% increase in range (from 50 km to 150 km), and a 300% increase in endurance (from 1.5 hours, to 6 hours). It is also reportedly capable of carrying underwing missile launchers. Although this capability has yet to be documented, it could likely carry any armament in a mode similar to the M2 and M4 variants described elsewhere.

It is unclear how the M2N achieves this increased range and endurance. The most likely explanation would be the addition of fuel tanks in the wings combined with weight reductions elsewhere (to explain the modest 5 kg increase in MTOW).

At the Kish Airshow, a poster showed the M2N fitted with wheeled landing gear even though the accompanying model was shown with the traditional skids.

M2N at Kish 2014 (military.ir)

Use:
In Iran, the Mohajer-2 is employed by the Army and IRGC for surveillance and attack. However, it is rarely documented in IRGC service – whether on exercise or parade – suggesting the majority are held by the Army. The majority of the Army's M2s have been documented in their ground forces. 17

In NEZAJA service, it is used for both high and low-intensity ISR. For high intensity conflicts, they are organized into or within UAV battalions to provide corps-level reconnaissance. Low intensity service includes routine border surveillance in support of ground operations, much the same way their significant helicopter fleet already operations. They are also used for non-military purposes, such as when the Army is mobilized to perform disaster relief during floods, earthquakes, or snowstorms.

The Raad-85 is expected to enter NEZAJA service in 2015, following its first tests during the Army's 12/2014 exercises. 18 Once it enters service, the Raad will be tasked with long-range strike missions. 19 This positions them alongside the NEZAJA's rocket artillery (e.g. Nazeats and Zelzals), which itself is a national-level force with a similar range (~100-300 km). Additionally, the NEZAJA is the only one of the Army's branches that will operate suicide UAVs, further widening the conceptual gap between the Raad and – for example – the role of the Air Force's PGMs, or the Navy's ASCMs. 20 21

Outside of the army, IRGC-GF was documented using a suicide strike variant during the Great Prophet 8 exercises in 02/2013.

Exports and Foreign Use:
Outside of Iran, the Mohajer-2 is operated by the Venezuelan Air Force, where they are known by their local name 'Arpia' (Harpy). They are assigned to the 83rd UAV Squadron, which is part of the 8th ISR Aviation Group based out of the El Libertador Airbase in Maracay. 22

Venezuela's acquisition of M2s began in 2007 when they inked an agreement with Iran that included UAV production. By 2009, the state-owned company CAVIM began assembling them from knock-down kits ships from Iran. 23 They were first unveiled to the public in 06/2012. 24 By 06/2013, CAVIM claimed to have produced 15 of them. 25 Three have reportedly crashed, leaving about a dozen in service. 26 In addition, an unknown number were delivered to a state-owned oil company – PDVSA – for pipeline inspections. 27
A Venezuelan Arpia up close (FAV Club)

Beyond Venezuela, there are some reports of the Mohajer-2 being sighted over Syria. However, the available imagery is inconclusive, and the M2 cannot be positively identified.

Recognition Features:



Mohajer-3 (M3) (Dorna):

Development:
The Mohajer-3 was announced alongside the the Mohajer-2 and 4 in 1999, presumably developed during the mid-90s. 28. It was supposedly designed as the initial attempt to extend the endurance of the M2. 29 It has not entered production, and was soon superseded by the Mohajer-4

The M3 is sometimes refered to as the 'Dorna', a reference to the crane bird.|

Technical Assessment:
The Mohajer-3 is a significant evolution of the Mohajer-2, and is characterized by its larger, squarish fuselage, and a redesigned tail section.

Specifications:
Speed, Cruise: 180 km/h
Range: 100 km
Endurance: 2-3 hours

Use:
There is no known operational employment of the Mohajer-3.

Recognition Features:



Mohajer-4 (M4) (Hodhod / Shahin)

Development
:
The Mohajer-4 was first referenced in 1999, when it was discussed alongside the M2 and M3. 30 It was documented photographically by at least 2003, possibly earlier. By the mid-2000s, more than 34 M4s had been produced (19 in ~2005, and 15 in ~2006), out of a total of 253 Mohajer-1/2/3/4s around the same time. 31

A new generation of M4 was unveiled in 09/2014, but has yet to supplant the current generation. 32

The M4 is sometimes referred to as the Hodhod, or Shahin. 'Hodhod' is a reference to the crested Hoopoe bird, which resides across Asia, Europe, and Africa, and is present in Persian mythology. 'Shahin' is a translation of 'falcon'. These designations are discussed further below.

Technical Assessment:
The Mohajer-4 continues the evolutionary path of the M2 and M3. Its larger size and aerodynamic refinements reflect its guiding design consideration: increased range and endurance.

Physically, the M4 is characterized by a) its square fuselage, and b) wings with a tapered trailing edge, canted wingtip, and a prominent fairing where they join the lower fuselage. Control surfaces are the same and include an elevator on the horizontal stabilizer, rudders on the vertical stabilizers, and ailerons on the wings.

Although a handful of early examples are powered by different engines, the Mohajer-4 is now uniformly equipped with the 50 hp Limbach L550 four-cylinder two-stroke engine fitted with a pusher prop. The examples equipped with different engines are typically painted in bright colors and lack markings, suggesting they are prototypes belonging to the Qods Company. The first of these is powered by an unknown 4-cylinder engine fitted with a carburetor superficially similar to that on the WAE-342. The second is fitted with the 38 hp AR-741 rotary engine. The reasoning behind choosing the L550 is opaque and may be due to specific circumstances such as availability. 33 One can speculate that the L550 – despite weighing more, and burning fuel at twice the rate of the 741 – was chosen foremost for its power, which would allow it to carry more fuel.

The Mohajer-4 is fitted with two antenna, typically arrayed on top of the avionics bay. Although the specifics of the system are unknown, it uses the same three modes found on the M2, which are described above. 34 Since the M4 enjoys a larger payload-capacity, and has more onboard power, it is a reasonable assumption that its functional control range is greater.

The M4 can be fitted with three different optical payloads: a) a fixed forward-facing camera in the nose for navigation, b) a gimbaled EO-system for surveillance, or c) a fixed downward-facing still camera for aerial surveying. The current-generation M4 can carry either the gimbal or survey camera, but not both. In practice, only daylight cameras have been documented in use. However, the next M4 generation (described below) can carry both types simultaneously, and has been shown fitted with a multi-channel imager. Even if these imagers were fielded immediately, their relative simplicity and lateness in arriving contrasts to the wide use of more sophisticated payloads in the similarly-sized AB3.

In 2014, the MoD revealed that the M4 could be equipped for air-defense with two QW-1 MANPADS. Lacking a dedicated system, these QW-1s would function much as they would on the ground. The operator would aline the tube with the target using onboard cameras, relying on the missile's own IR-seekers to acquire the target. Although its easy to see where this could be useful – for example, against a lone helicopter presenting itself as a target of opportunity – this system has not turned the Mohajer into a dedicated interceptor by any means.

Specifications (Mohajer-4*): 35
Length: 3.64 m
Wingspan: 5.30 m
Weight, MTOW: 175 kg
Max Speed: 180 km/h
Endurance: 3-5 hours
Ceiling: 4,500 m
Range: 150 km

* Unknown powerplant fitted to associated model.

Specifications (Hodhod A/100*): 36
Length: 3.74 m
Wingspan: 5.3X m (where x=2, 3, or 4)
Weight, MTOW: 210 kg
Speed: 200 km/h
Endurance: 3 hours
Ceiling: 4,500 m
Range: 150 km

* Shown fitted with rotary engine. See description below.

Variants:

Hodhod A/1 [A/100]:
It is unclear whether the 'Hodhod' designation applies to a specific variant with unique characteristics, or something else. One plausible explanation is that it is name used by the IRGC, while another plausible explanation is that it is an M4-variant with slightly different physical specifications.

Two specific cases have been documented:

First, in 09/2010, the designation was applied to a display model fitted with with the AR-741 engine, and painted in a bright red and white paint scheme. The accompanying placard produced by the IRGC included unique specifications that differed from those usually attributed to the M4. Specifically, it claimed that the Hodhod is slightly longer than the M4, has a slightly wider wingspan, has a larger MTOW, and possibly a shorter endurance. Because these differences are inconsistent with the use of the AR-741 in place of the more powerful L550, it is a reasonable working assumption that the 'Hodhod' designation does not refer to a variant powered by this engine. 37

Second, during a parade in 09/2010, it was applied to two M4s operated by the IRGC. These two were identical to other M4s except for a unique serial format, and – possibly – a new payload bay under the fuselage. Unlike the first case, they were fitted with the L550 and lacked the 'A/1' or 'A/100' suffix in their designation.

Shahin:
Like the Hodhod, it is unclear whether the 'Shahin' designation refers to a specific variant, or is a service-specific designation.

The designation was first applied to a NEZAJA M4 on parade in 09/2010. By 10/2013, media sources were referring to it as a specific M4 variant, and suggesting – albeit, ambiguously – that it was NEZAJA-specific. 38 This source also noted that the Shahin's MTOW was 230 kg, higher than most descriptions of the M4's MTOW.

However, this claim is difficult to assess because the media may have based this claim entirely on the 09/2010 imagery, potentially creating a circle of erroneous confirmation based on trust in 'official' sources like Fars and Mashregh News. This is exacerbated by the tendency of most major agencies to copy and paste whole sections from preexisting articles. For example, sections from the 10/2013 article were reproduced in reports ostensibly talking about the Shahin's participation in a 12/2014 exercise, creating the illusion of independent confirmation. 39

Sadiq / Mohajer-4B:
The Sadiq – or Mohajer-4B 40 – is a significant evolution of the M4 platform that was unveiled during a defense industries exhibition in 08/2014. No performance information is available.

There is some uncertainty over its designation because they were unveiled alongside two related MoD projects (aerial-survey and air-defense payloads). However, given the payload's parallel use on current generation M4s, it is a reasonable assumption that the M4B is a stand-alone development. It is possible that the 'Sadiq' designation may refer to any M4 equipped with the specific aerial-survey payload.

Physically, the Mohajer-4B can be recognized by:
- New landing skids
- Wings mounted midway on the fuselage; canted wingtips removed; wider span possible.
- Fuselage reshaped for better nose aerodynamics, and improved engine cooling. 41
- Expanded payload bays can now carry gimbaled and downward-facing cameras at the same time.
- Undetermined payload may be associated with new housing on the bottom fuselage.

Use:
In Iran, the M4 is employed by the Army and the IRGC for high and low intensity ISR. They are known as the Shahin in the Army's Ground Forces, and appear to be organized similarly to the M2. 42 The Ground Forces have used M4s since at least 2010 and took delivery of a significant number in Fall 2013, emphasizing their use in border security. In November 2014, one of the M4s documented earlier on parade (SN: A041-112) was downed by the Islamic State during a surveillance flight over Diyala, Iraq. Notably, this particular UAV included a tail-boom from a different kit (SN: A041-66), which itself was documented during the 2013 delivery as part of another mixed kit, illustrating the modular nature of the M4's components.

Although they have not been confirmed in use by the IRIAF, IRIN, or IRIADF, an M4 was shown in the Persian Gulf during 2010's Velayat-89 exercise, which is typically associated with the Army's air and naval forces.

They are also used for maritime surveillance by the IRGC, who have published videos of their M4s documenting the transit of international warships through the Strait of Hormuz. Among other uses, the IRGC also employs them for internal security in places like Sistan & Baluchistan alongside the force's own Shahed UAVs.

Exports and Foreign Use:

Outside of Iran they have been documented in use over Iraq and Syria, though it is not always clear who is operating them. A handful have been reported in flight over Syria since 2012, but these may be misattributed AB3s, which are far more common. However, an M4B was shot down over Deir az-Zohr in January 2015 and recovered.

In Iraq, in addition to the Ground Force's M4 described above, at least two more M4s have been lost in action. The first of these was recovered near the city of Samarra in July 2014, and the second was recovered near Kirkuk in January 2015. In the second case, the M4 bore no identifying markings, but in the first case carried several Iraqi flag decals.

Recognition Features:



Appendix: Documented Airframes and Serials:

Mohajer-2:
MX2-009 (IRGC, Great Prophet 8)

Mohajer-4:

A041-44 (09/2011)
A041-63 (04/2009)
A041-65 (09/2013) (NEZAJA)
A041-66 (09/2013) (NEZAJA)
A041-67 (unknown)
A041-80 (2010)
A041-81(?) (04/2010)
A041-90 (12/2014) (NEZASA)
A041-92 (09/2013) (NEZAJA)
A041-108 (09/2013) (NEZAJA)
A041-111 (09/2013) (NEZAJA)
A041-112 (09/2010, 11/2014) (NEZAJA)

120 (07/2014) (Iraq)

A041-A/B119 (08/2014) (unknown)
A041-A/B201 (01/2015) (Iraq/unknown)

TUAV-M4B-08 (SDW 2010)

Mohajer-4B:
P062A-007 (M4B) (Syria/unknown)

Footnotes / Works Cited
:

1) There is a handful of imagery, which shows an M1 being recovered by parachute, that appears to be genuine.
2) Image gallery and additional information about the movie available at Soureh Cinema and War is Boring
3) Past and Current UAS Activities in Iran. UAS Yearbook 2009.
4) ibid UAS Yearbook, 2009
5) A Look at the Role of the Mohajer and Tallash in Karbala-5 and Valfajr-8. Mashregh News. 10/11/2011
6) Iran-Iraq War in the Air 1980-1988. Tom Cooper and Farzad Bishop. Schiffer Military History. 2000. p.196, 235
7) The original source for this claim has since been lost, and may only be apocryphal.
8) Cooper and Bishop, 2000. p.196
9) Iran Exhibits Advanced Aircraft and Drones. IRIB. 07/19/1999.

    Summary archived at: Iran Missile Chronology. NTI. 08/2011.
10) It is very likely that the M2 appeared in earlier exhibitions, including Kish 2002, but the lack of currently available imagery from these events makes it impossible to confirm at this point.
11) DM: Raad and Nazir are two aircraft with offensive power and maneuverability … [unclear] ISNA. 02/08/2011
12) Saeqeh and Toofan for the Enemies; Sofreh Mahi for Future Generations. Mashregh News. 10/19/2011
13) Production of the Raad-85 Suicide UAV in the Army Ground Forces. YJC. 09/28/2013.
14) Commander: Iranian Ground Force's Drones Make 150 Flights in 1 Year. FNA. 09/28/2013
15) Targeting at 250 km with Suicide UAVs. AJA. 12/2014.
16) It is assumed that two different practices are used when describing the respective ranges of reconnaissance and suicide UAVs. The 250 km one-way range of Raad is close to the M2N's 300 km one-way range, allowing for extra payload weight.
17) It is possible that this documentation is only a reflection of circumstances, and do not reflect the actual distribution of equipment.
18) Suicide UAVs Used for the First Time in the Mohammed Rasoolallah Exercise. AJA. Date Unknown, 12/2012 suspected.
19) NEZAJA's UAV Group's Fleets Ready to Enter Asymmetric Battle Space. AJA. Date unknown, Fall 2013 suspected.
20) Using Suicide UAVs in the Army's Exercise. IRDiplomacy. 12/25/2014
21) Suicide with the Yasir; the NEZAJA's [RQ-7 Shadow]. Tasnim News. 01/06/2015
22) http://www.fav-club.com/qods-aeronautics-industries-mohajer-2-cavim-sant-arpia/
23) A handful of current and former CAVIM employees with profiles on LinkedIn list work experience relating to the Mohajer beginning in 2009.
24) Venezuela-Iran UAVs. Jeffrey Lewis. Arms Control Wonk. 06/12/2012
25) http://www.fav-club.com/qods-aeronautics-industries-mohajer-2-cavim-sant-arpia/
26) Iranian Mohajer-2 Drone Appears in Venezuela. Chavez's Building His Own Drone Fleet with the Help of Tehran. The Aviationist. 06/12/2012.
27) ibid CAVIM employees' LinkedIn profiles.
28) ibid IRIB, 1999
29) The Mohajer 3 and 4 [Mark] Iran's Entry Into the Major League of UAVs. Mashregh News. 10/10/2011
30) ibid IRIB, 1999
31) Official production data presented during public expo in mid-2000s. Via MATF
32) Mohajer and Misagh; a Combination That Will Break Any Evil Intentions. Mashregh News. 09/23/2014
33) Around the same time period (late-90s/early-00s), the AB2 was advertised with a rotary engine as well, but has only ever been produced with the two-stroke WAE-342. Only more recently has the rotary AR-741 begun to show up as the standard engine in some of the smaller Shahed-series.
34) The Most Famous Iranian UAV Family Documented Again / Mohajers Looking for Air Targets. FNA. 09/23/2014.
35) MATF, SDW 2011
36) Mohammed Hussein, SDW 2010. HT @ AminCo at IMF
37) Although, as a general rule, 2-stroke engines consume less fuel and are offer less power for their size and weight than rotary engines, the L550's greater power (50 hp vs 38 hp) flips these characteristics. This means that one would expect to see this 'Hodhod' (which is fitted with the 38 hp AR-741) have a lower MTOW, and longer endurance.
38) The Heavy Shadow of the “Shahin” on the Borders / Eyes that See Blind Spots. FNA. 10/19/2013.
39) Shahin Flight; Heaviest NEZAJA UAV in the Big Army Exercise. FNA. 12/25/2014
40) The notional designation is based off a) the explicit labeling of this UAV as a “Mohajer-4”, combined with b) the unique characteristics distinguishing it from current-generation M4s. The specific origin of the “-4B” designation is a poster displayed in the mid-2000s showing the progress of various projects being undertaken by the Qods Company. One such project was the Mohajer-4B, whose development was reportedly 95% complete.
41) ibid Mashregh News, 09/23/2014
42) ibid FNA, 10/19/2013