Shahed 285 (AH-85)
The Shahed-285 is a light-attack/observation helicopter designed by the Shahed Aviation Industries Research Center (SAIRC), a subset of the Iran Aircraft Manufacturing Industrial Company (http://thearkenstone.blogspot.com/HESA), in cooperation with the Revolutionary Guards.
![]() |
| AH-85A (Mashregh News) |
Role:
The Shahed 285 has obviously been designed as a "budget" helicopter, almost everything about it is cheap and easy to produce; this necessarily has it's trade-offs and isn't inherently a good or a bad approach. According to reports by Mashregh News, the AH-85 is tasked with scouting out enemy locations and because of their light armor and high speed, attack targets of opportunity. (1) The underlying implication here is that it's not meant to replace the AH-1, it's meant to supplement them in the same way OH-58s supplement AH-64s in the US Army.
Development:
![]() |
| Zafar-300 at the Tehran Aviation Museum (Vahid Moghadem) |
Meanwhile during the late 1990s and early 2000s Iran's own reverse-engineered AB-206, the Shahed 278, was maturing and by the early 2000s a handful has been produced. It's clear that sometime during this process that the thought turned toward arming it because Jane's reported that in 2005 Iran had tested the "OH-78". Unfortunately at this point it gets somewhat confusing. Jane's reports that the helicopter in question is a light recon helicopter converted from the second protype Shahed 278. It is powered by the Allison 250-C20 and is armed with a chin-mounted 7.62 mm machine-gun and 70 mm rockets. Most notably of all perhaps though is that Iran claimed they were using thermal optronics from the French company "Saqem" which provides the imaging capability for the Eurocopter Tiger. Moreoever, they claimed to be producing them in Iran! (3)
Jane's also reported that Iran was also developing another helicopter, the Shahed 478 which would feature four slightly longer rotor blades and a more powerful 250-C30R engine procured legally through Canada. This meant that it would now have a gros weight of 2,040 kg and be able to carry 1,000 kg worth of weaponry. Jane's also reported a drawing of the new helicopter which the author describes as showing C-704/Nasr missiles. (4)
Both of these projects sound very similar to the Shahed 285 concept and there are several explanations that might explain this similarity:
![]() |
| Supposed OH-78 |
2) The Shahed 285 was the culmination of the OH-78 and 478 - In the same way the final version of the Shahed 278 was preceded by a couple different Bell 206 reverse-engineering attempts, it's entirely possible that the AH-85 simply represents the final design path chosen by the engineers for reasons that we can only guess at.
3) The Shahed 285 was a forced compromise - Both the OH-78 and Shahed 478 are remarkable in that they both rely on foreign components for critical systems; the OH-78 uses French optics and the 478 uses Canadian engines. It's possible that the relations established pre-2006 broke down and forced Iran to design a helicopter with more modest capabilities that represented a compromise between the lightly armed OH-78 and the more advanced 478. It may also be because the 478 cost too much and the AH-58 represents the budget choice for the IRGC.
The Shahed 285 is notable in that is inferior to the 478 (two versus four rotor blades and without the uprated engine) which indicates a combination of all three might be the most likely possibility. The 285 may very well represent a progression of the OH-78 that evolved in light of the inability or unwillingness to produce the more powerful 478. Thus the final helicopter, while still carrying the 250-C20 engine, has been slimmed down and optimized for the light attack role.
Finally, in May 2009, two Shahed 285s were unveiled to the public in a ceremony featuring Shahed 278s as well. Then in November 2010 the same two helicopters, albeit in an updated configuration, were shown during the Kish Island trade and air show.
Design:
While it might have originated as a Bell 206, the final AH-85 bears a number of important differences. Most noticeably, the entire fuselage has been given the profile of a traditional attack helicopter by removing the small passenger compartment and position for a second crewman and replacing it with fuel tanks and a small storage area which is contained within a very narrow, vertical-sided body. It is supposedly significantly taller then the Shahed 278 but this cannot be visually verified.
![]() |
| Side-by-side comparison of Shahed 278 and 285 (adapted from Mashregh News) |
The pilot sits recessed in the fuselage unlike the bubble canopy of the Bell 206 which logically translates into reduced viability. The cockpit uses the basic instrumentation configuration from the Shahed 278 though additional controls can be found running along the left and right hand side of the cockpit.
Located directly above the cockpit is a mounting spot for optronic devices like the French FLIR mentioned in conjunction with the OH-78. Low-quality images have confirmed the presence of a device but cannot indicate whether it is the elusive French optics or an indigenous equivalent, perhaps one of IEI's EOG systems. (5)
On top of the fuselage are the distinctive engine air intakes as well as the exhaust outlets which betray the identity Allison 250-C20/C20B engine.
The tailboom section is straight from the Shahed 278 which places the h-stab at the top of the v-stab which forms a "T" shape rather then being located on the tail boom like on the 206.
On the side of the fuselage, about where the passenger doors would be on the 206/278, are two weapons pylons with hard-points for various weapons.
The body is built of of "non-metallic composite components" which indicates materials like fiberglass, kevlar or other bullet-resistant fabrics, and even some of the lightweight ceramics though latter are exceptionally expensive. (6)
This fact, combined with the flat panels and apparent lack of 90-degree angles have led some to claim that the helicopter is stealthy. While it is true that these types of materials don't reflect radar waves as effectively as metal surfaces, the helicopter still has a number of "stealth-killing" features like exposed rotor blades. landing skids, weapons pylons and V/H-stabs.
Performance:
The Shahed 285 prototypes are powered by the Allison 250-C20 engine while the production models are scheduled to be fitted with the more powerful 250-C20B which can be identified by the air splitter on the intakes for the engine which cannot be seen on the prototypes. Iran has been caught before attempting to import 250-C20-variant engines before so it's unknown what the current level of capacity is for indigenous production of the engine components. (7)
![]() |
| Air-splitter an an AB-206B (right) versus an AH-85A (left) |
This drives a main rotor assembly taken from the Shahed 285 as well as a tail rotor.
With regards to performance, the helicopter falls in the middle of the road with most of it's specifications like service ceiling and cruising speed resembling the Bell 206 It does have an above average range though, thanks in part to the one-man crew which allows it to carry additional fuel.
Importing the drive system directly from the Shahed 278 rather then going with the more powerful one planned for the Shahed 478 (or something comparable) was easy enough and has real short and long term cost cutting benefits, but it also means reduced potential performance and an increased radar signature.
Armament:
As a light attack helicopter, the Shahed 285 carries a modest armament for self-defense and targets of opportunity. There are several different configurations which generally correspond to the helicopters sub-variant.
![]() |
| AH-85 - note the exposed gun and EO payload (Mohammed Hussain) |
The SUU-11 gun pod is another candidate judging from their use on other IRIN/IRIAA helicopters but have not been actually seen.
The heavy AH-85B has not been seen yet so we can only guess at what a heavier version of the AH-85A might be armed with; possibilities include some kind of ATGM, or heavier gun-pods.
| AH-85C with Kowsar (YT) |
![]() |
| AH-85C with Sadid-1 (Kambiz Noori) |
The missile itself is fired from a canister which is about 1.5 m long and 15 cm in diameter. Though it must be emphasized that these are just numbers obtained from "eyeballing" it. This puts it on the relatively small end of things for a missile with a 10 km range. It's probable that this rather exceptional range is due to an aerial launch or is an exaggeration. If it were true however it would probably mean that the warhead would be relatively light.
The stencils "AIRC" indicate that it may have exclusively designed for the use as an airborne weapon system rather then generic ATGM.
Variants:
At the time of this writing, two different airframes are known to exist, one AH-85A and another AH-85C; a total of six are reported to exist with the final four undergoing flight trials as of late-2010. (10)
AH-85A - Light overland version. It is intended for low-intensity policing conflicts or border patrol. Armed with a 7.62 mm machine-gun in the nose and two 70-mm rocket pods on hard-points.
AH-85B - Heavy overland version. Although it has yet to be seen, this model is said to be intended for "non-symmetrical wars". (11) Nothing further is known.
AH-85C -Naval attack version. Equipped with a basic surface-search radar in it's nose instead of a machine-gun. Also equipped with a slightly different cockpit configuration then the AH-85A. Armament includes either two Kowsar AShMs or eight Sadid-1 missiles.
Specifications:
AH-85
Crew: 1
Length: 11.84 m
Width: 2.78 m
Height: 3.42 m
Rotor Diameter: 10.16 m
Tail Rotor Diameter: 1.57 m
Empty Weight: 820 kg
Max Take-Off Weight: 1,450 kg
Service Ceiling: 4,160 m
Max Rate of Climb: 7.6 m/s
Cruising Speed: 225 km/s
Endurance: 5 hours
Range: 800-890 km
Works Cited:
(1) ibd Mashregh News, 2011
(2) Zafar 300. Jane's Intelligence. http://articles.janes.com/articles/Janes-All-the-Worlds-Aircraft/ZAFAR-300-Iran.html
(3) Iran Plans Armed Helicopters. Jane's Defence Weekly. Robert Hewson. December 20th 2006.
(4) ibd Hewson, 2006
(5) For example: http://www.ieimil.ir/content/electro-optical-gyro-stablized-surveillance-system-eog
(6) ibd Mashregh News, 2011
(7) Firm Accused of Illegal Aircraft Exports to Iran. The Washington Post. March 25th 2009. http://www.washingtonpost.com/wp-dyn/content/article/2009/03/24/AR2009032403238.html
(8) شاهد285 شمشیر بُرنده سپاه+عکس. Mashregh News. Winter/Spring 2011. http://mashreghnews.ir/NSite/FullStory/?Id=36364
(9) ibd Mashregh News, 2011
(10) Shahed 285. Iran Military Forum. Post #154. November 20th 2010. http://www.iranmilitaryforum.net/index.php?topic=734.msg56377#msg56377
(11) newest variant of iranian made Shahed 285 light attack helicopter. Iran Defense Forum. Post: #11. November 11th 2010. http://www.irandefence.net/showpost.php?p=924223&postcount=11








Very in-depth! Thank you
ReplyDeleteAs always, a wonderful article. I'm going to edit wikiran as soon as possible.
ReplyDeleteas Aspahbod Said, like always very good article.
ReplyDeleteGalen do you have any source for this?:
"The Shahed 285 prototypes are powered by the Allison 250-C20 engine while the production models are scheduled to be fitted with the more powerful 250-C20B".
have you noticed to difference of land and naval version in top section of body?
M-ATF
ReplyDeleteThe max engine power has been advertised as 420 hp which matches the 250-C20B as compared to the 400 hp 250-C20. However the two prototypes seen thus far are lacking the air-splitter found on Iran's AB-206s with the 250-C20B. Check out the picture below the text that you quoted and you'll be able to see the difference.