Mil Helicopter Company List

[hesham]

Hi,

Mil was established in 1947 under the guidance of Mikhail Mil as the helicopter
laboratory of the Central Aerohydrodynamic Institute in Zhukovsky, Moscow
Oblast.

Mil merged with Kamov and Rostvertol to form Russian Helicopters in 2006.
The Mil brand name has been retained, although the new company eliminated
overlapping product lines.

I will talk about them,it's list contains,

Mi 1,2,3,4,5,6,7,8,9,10,11 ?,12,14,15 ?,16,17,18,19,20,21,22,24,25,26,27,
28,30,32,34,35,36,38,,40,42,44,46,48,50,52,53,54,58,60,115,171,172,173,
234,329,381,382,383 & 450

 

[hesham]

Here we go,

EG-1 was an experimental helicopter project of 1945,led to GM-1
GM-1 was the original designation of the Mil Mi-1 prototypes, powered by a AI-26GR 500–550 hp radial engine,1948
Mi-1 was a light multi purpose helicopter 1949,powered by one 550 hp AI-26V radial engine
Mi-2 was a larger multi purpose helicopter,one crew and eight passenger,powered
by two 400 shp Isotov GTD-350 turboshaft engines
Mi-3 was the same as Mi-1KR,1954
Mi-3/II was the same as Mi-1S,with 4-bladed propeller, experimental (ambulance version with 2 easily removable nacelles on the sides of the fuselage),1955
Mi-3/III was developed from Mi-2 With the increase in cross section of
the fuselage,the rear cargo doors of the cab. Project, 1964 (with two
GTD-350 engines).
Mi-3/IV was light multipurpose,together with Poland-based development
of the Mi-2. Project 1971 (with two GTD-850 engines)
Mi-4 was a medium transport helicopter,had oe or two crew and 16 troops,powered
by one 1680 shp ASH-28V 14-cylinder air-cooled radial piston engine
Mi-5 was a project of light helicopter powered by one 750 hp engine and
had a takeoff weight of 2400 kg,developed from Mi-1 in 1957
Mi-6 was a heavy and large transport helicopter,crew of six and had a capacity
of 90 passengers / 70 airborne troops / 41 stretcher cases with 2 medical
personnel,powered by two 3100 shp Soloviev D-25V turboshaft engines
Mi-7 ?,was probably the same as V-7,as an experimental light four-seat
helicopter,powered by one AI-7 ramjet engines
Mi-8 Early Concept was a multi-purpose medium transport helicopter,powered
by one 1900 shp engine
Mi-8 was later developed from previous one,had crew of three and 24 passenger,
powered by two 1950 shp Klimov TV3-117MT turboshaft engines
Mi-9 was a developed version of Mi-8,with increased fuel capacity and onboard communications system,1977
Mi-10 was a huge skycrane helicopter,crew of three and 28 passenger, powered
by two 5500 shp Soloviev D-25V turboshaft engines
Mi-11 was a tandem-rotor heavy transport project,had a wing and maybe
appeared in late of 1950s
Mi-12 was a largest helicopter ever built,crew of six and 195 passenger,powered
by four 6500 shp Soloviev D-25VF turboshaft engines
Mi-13 was an Electronic jamming version based on the Mi-8MT
Mi-14 was an anti-submarine warfare helicopter,with crew of four,powered
by two 1950 shp Klimov TV3-117MT turboshaft engines
Mi-15 ? was unknown,but may it was a super-heavy flying crane helicopter project with 60 m diameter main rotor,late 1950s
Mi-16 ? was unknown,but may it was the same as V-16,a helicopter project of
side-by-side twin rotor design with two high-power turboshafts, low-rotating turbines and vertical shafts,powered by six Soloviev D-25VF turboshaft engines
Mi-17 was a military transport version of Mi-8,with a refine shape
Mi-18 was a prototype lengthened version of Mi-17
Mi-19 was an Airborne command post variant of Mi-17
Mi-20 was a super light helicopter project,mockup only, powered by one
TVD-10A engine
Mi-21 ? was unknown and probably not used,but may it was a light experimental helicopter with turbojet engines at the tips of the 5 blades
Mi-22 was a military command support variant of Mi-6
Mi-22/II was a 1965 Soviet project to develop a military transport helicopter,
it was a development of the Mi-2,powered by one 940 GTD-10A turboshaft
engine
Mi-23 ? was unknown,probably not used,but may it was a twin tilt-rotor project
of 1964,looks like Bell XV-3.
Mi-24 Early Concept was the same as the follow one,but powered by one 2200 shp Isotov TV3-117 turboshaft engine
Mi-24 was a heavy combat and transport helicopter,crew of two and 8 troops,
powered by two 2200 shp Isotov TV3-117 turboshaft engines
Mi-25 was exported version of Mi-24
Mi-26 Early Concept was two screw transverse design heavy transport helicopter
project,powered by four D-136 turboshaft engines
Mi-26 was a heavy transport helicopter, world's heaviest helicopter,crew of five
and 90 troops,poweed by two 11400 shp D-136 turboshaft engines
Mi-27 was proposed as Airborne command post variant of Mi-26
Mi-28 First use was a rotary wing attack aircraft project, 1968,based on the Mi-24 (without cargo cabin)
Mi-28 was a tandem two-seat attack helicopter,powered by two 2194 shp
Klimov VK-2500 turboshaft engines
V-29 was a prototypes version,led to develop Mi-26
Mi-30 was a tilt-rotor STOL/VTOL convertiplane aircraft project of 1972,the first
design powered by three Isotov TV3-117F engines
Mi-32 was a three rotor super heavy helicopter project,powered by six D-136
engines
Mi-34 was a four-seat multi-purpose lightweight helicopter,powered by one
Vedeneyev M-14 radial piston engine
Mi-34V was twin engined version of Mi-34,powered by two TBL-450 engines
Mi-35 was also an export version of Mi-24
Mi-36 was a multi-purpose lightweight helicopter project of early 1980s,powered by two Isotov TV-O-100 engines
Mi-37 is the same as V-37, a modern medium transport helicopter project,please see reply # 28
Mi-38 was a transport helicopter,with a refine configuration,powered by two 2800
shp Klimov TV7-117V turboshaft engines
Mi-40 was an armed utility transport project version of Mi-28,powered by two
Klimov TV3-117VM engines
Mi-42 was a projected assault/transport helicopter featuring the NOTAR concept,
powered two GTD engines
Mi-44 was a utility helicopter based on the Mi-34,powered by two TBL-450 engines
Mi-46T was the passenger/cargo transport version, built similar to the Mil Mi-26, with a takeoff weight just half the weight of the Mi-26, fit to replace the aging Mi-6. The Mi-46T requires two new-type Aviadvigatel turboshaft engines, each with a power of 5,590 kW
Mi-46K a flying crane version,it was fit to replace the Mi-10K, and is designed similar to it, with a crane styled construction similar to the Mi-10K with stub wings,and long braced landing gear. D-21SV engine PD-12V turboshaft. However, its development is hindered by the lack of an engine, as until now there is no suitable engine for this helicopter. The Mi-46K requires two unspecified 5,965kW turboshaft engines
Mi-48 ? was unknown design,probably not used
Mi-50 ? was unknown design,probably not used
Mi-52 was a a projected four-seat light utility helicopter of the 1990s,powered
by one VAZ-4265 engine
Mi-53 was a military attack and light transport helicopter as Hind III
Mi-54 was a civil utility multi-role helicopter project,crew of two and 10-12 passenger, powered by two 771 shp AL-32 turboshaft engines
Mi-56 ? was unknown design,probably not used
Mi-58 was a projected twin-turbine passenger helicopter based on the Mi-28,
powered by two Klimov TV3-117VMA-SB3 turboshaft engines
Mi-60 was a joint project between Mil and the Moscow Aviation Institute to develop a light utility helicopter,powered by one 237 shp VAZ-426 engine
Mi-115 was a helicopter project,no more details
Mi-171 was an export version of the Mi-8AMT
Mi-172 was a civil passenger version manufactured in Kazan plant and based on the Mi-8MTV-3
Mi-173 ? was in my files,without any details ?
Mi-234 was a version of Mi-34 powered by VAZ-4265 piston engine
Mi-240 ? was a helicopter transport project,called P-240,need confirm on designation
Mi-329 ? was in my files,as a variant of Mi-17,need confirm or explanation
Mi-381 was a western version of the Mi-38, powered by Pratt & Whitney PW127TS engines
Mi-382 was a Russian version of the Mi-38, powered by Klimov TV7-117V engines
Mi-383 was a refine and military version of Mi-38,project
Mi-450 is a high speed rotary-wing aircraft project concept
Mi-



- To be continued

 

[hesham]

I reach to Mil Mi-22.

 

[hesham]

Up to Mi-30

 

[hesham]

Raising up to Mi-50 ?,and I add some projects and prototypes to the
list.

 

[Stargazer]

A lot of sub-versions missing in your list. Were you planning to add them later?

• Mi-1, Mi-1MNKh, Mi-1T
• Mi-2, Mi-2D, Mi-2FM, Mi-2P, Mi-2RL, Mi-2RM, Mi-2URN, Mi-2URP, Mi-2URP-G, Mi-2URС, Mi-2US, Mi-2Kh, Mi-2Sh
• Mi-4, Mi-4A, Mi-4P
• Mi-6, Mi-6P
• V-7 remained V-7 and was never turned into an "Mi-7" designation.
• Mi-8, Mi-8 (military "Hip-C"), Mi-8AMTSh, Mi-8MT, Mi-8MTKO, Mi-8MTV, Mi-8MTSh, Mi-8SP, Mi-8T
• Mi-10, Mi-10K
• V-12 remained V-12 and was never turned into an "Mi-12" designation.
• V-16 remained V-16 and was never turned into an "Mi-16" designation.
• Mi-17 ("Hip-H"), Mi-17PP ("Hip-H"), Mi-171, Mi-171A
• V-24; Mi-24V Krokodil, Mi-24V, Mi-24F, Mi-24A ("Hind-A"); A-10; Mi-24U ("Hind-C"), Mi-24B, Mi-24BМT, Mi-24VМ, Mi-24VP, Mi-24D, Mi-24DU, Mi-24K, Mi-24P, Mi-24PN, Mi-24T
• Mi-26, Mi-26NEF-M, Mi-26PK, Mi-26TM, Mi-26T2
• Mi-28, Mi-28N
• Mi-35 ("Hind-E"), Mi-35M, Mi-35P
• Mi-38, Mi-382

NOTE: this is only the result of my research and is probably not complete.

 

[hesham]

Of course I delay the variants to another posts,but we have already
Mi-8 here,

https://www.secretprojects.co.uk/threads/the-extended-family-of-the-mil-mi-8.19941/

 

[hesham]

I complete it,and additions or corrections are welcome.

 

[AM]

I complete it,and additions or corrections are welcome.

Hi

My list of Mil' helicopters (only in Russian)

 

[hesham]

Thank you my dear AM,but I can't read it at all,it appeared like this.

For Mi-1 Variants;

- GM-1 with one AI-26GR engine,liaison helicopter with 3 blades main rotor,1948
- GM-1 with one AI-26GRF engine,experimental helicopter of 1949
- GM-1 (Mi-1) with one AI-26GR engine, as a military helicopter1950
- GM-2 with one AI-26GRF engine,as experimental trainer two-seat helicopter,1950
- Mi-1U with one AI-26GR engine,as a trainer helicopter 1951
- Mi-1 with one AI-26GR engine,a sa light multi purpose helicopter 1952
- Mi-1 (GM-3) with one AI-26GRF engine,as an experimental helicopter 1952
- Mi-1T was a three-seat general-purpose transport helicopter, seating a pilot and two passengers, powered by one AI-26V radial piston engine 1954
- Mi-1 with one AI-26V engine,as a communication helicopter 1954
- Mi-1KR as Mi-3 of 1954
- Mi-1TKR was a light reconnaissance and liaison helicopter of 1956
- Mi-1NH or NHK was a three-seat general-purpose utility helicopter, basing
on Mi-1T,1956
- Mi-1ASW was anti-submarine helicopter of 1955
- Mi-1T (Second use) was a military telephone line installer,1957
- Mi-1A was a three-seat general-purpose transport helicopter of 1957
- Mi-1U/TU/AU/MU was a Dual-control training helicopter variants 1957
- Mi-1AKR was a light reconnaissance and liaison helicopter, basing on Mi-1A
- Mi-1S with 4 blades,as an ambulance version 1955,(Mi-3/II)
- Mi-1M was a four-seat light general-purpose helicopter of 1957
- Mi-1MNKh was a four-seat general-purpose utility helicopter, basing on Mi-1M,1957
- Mi-1M Moskvich was a Civil transport helicopter for Aeroflot, with better cabin soundproofing, equipped with hydraulic controls and an all-metal rotor
- Mi-1MG was a float-equipped version of the Mi-1M for whaling ships, of 1958
- Mi-1MU First use was a Dual-control training helicopter 1958
- Mi-1MRK was a prototype of a liaison helicopter, basing on Mi-1M,1959
- Mi-1KF was a float-equipped version of Mi-1MG 1960
- Mi-1MU was a prototype of an armed variant, tested from 1961
- Mi-1MUs was an experimental many variants with various bombs
- Mi-1V was an attack helicopter,powered by one AI-26V engine
- Mi-1M Second use was a version for special forces,5 troops,Project 1960
- Mi-1KF was a float helicopter (conv. Mi-1MG),1963
- Mi-1Exp was a light experimental helicopter with turbojet engines at the tips of the 5 blades,powered by one AI-7 engine,Project 1965

I don't prefer to speak about Polish versions.

Mil Mi-1 - Wikipedia

en.wikipedia.org

*** To be continued

 

[AM]

Thank you my dear AM,but I can't read it at all,it appeared like this.

For Mi-1 Variants;

- GM-1 with one AI-26GR engine,liaison helicopter with 3 blades main rotor,1948
- GM-1 with one AI-26GRF engine,experimental helicopter of 1949
- GM-1 (Mi-1) with one AI-26GR engine, as a military helicopter1950



*** To be continued

 

[hesham]

For Mi-2,

- V-2 was an experimental light helicopter and medium transport,powered
by two GTD-350 turboshaft engines,1960/61
- V-2 was an agricultural helicopter,powered by two GTD-350 turboshaft engines
of 1962
- V-2 was a transport helicopter project with 10 passenger,powered by two
GTD-350 turboshaft engines of 1964
- V-2M was a marine helicopter version,with emergency inflatable balloons,
powered by two GTD-350 turboshaft engines of 1965
- V-2V was an armament prototype,also powered by two GTD-350 turboshaft
engines
- V-2 was a version ,with a comfortable salon,1967
- Mi-2 was another combat helicopter,powered by two GTD-350 turboshaft
engines of 1965
- Mi-2T was a multi-purpose light helicopter,powered by two GTD-350 turboshaft engines of 1965
- Mi-2S was an ambulance version,powered by two GTD-350 turboshaft engines
of 1965
- Mi-2SR was also an ambulance and rescue version,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2Ch was an agricultural helicopter as a Polish version,powered by two
GTD-350 turboshaft engines of late 1960s
- Mi-2P was a passenger and cargo version, with accommodation for 6 to 8 passengers,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2P Salon was a comfortable salon,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2Sh/Mi-2U/UMi-2/Mi-2SZ were a dual control trainer versions,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2M with a 4 bladed and enlarge fuselage,project of 1967,but powered
by two "GTD-550" turboshaft engines
- Mi-2M1 was a version with gas turbine,1968
- Mi-2RM was a sea rescue version equipped with electric winch for two people and dropped rafts,powered by two GTD-350 turboshaft engines of 1969
- Mi-2RL was a land rescue and ambulance version,powered by two GTD-350 turboshaft engines of 1969
- Mi-2F was a photographing and mapping version,powered by two GTD-350 turboshaft engines of 1969
- Mi-2FM was a survey version,powered by two GTD-350 turboshaft engines of 1969
- Mi-2 was a flying laboratory version,1971
- Mi-2US was an Armed version fitted with a fixed 23mm NS-23 cannon, 4 x 7,62mm PKT machine gun pods and optional cabin PK machine gun,1970/71
- Mi-2URN was an Armed variant with a fixed 23mm NS-23 gun and two 16x57mm S-5 unguided rocket pods Mars-2. Optional 7,62mm PK machine gun window-mounted,1971/72
- Mi-2URP was an Anti-tank variant, armed with 23mm NS-23 gun, optional window-mounted 7,62mm PK machine gun, and 4x AT-3 Sagger (9M14M Malutka) wire-guided missiles on external weapons racks and 4x additional missiles in the cargo compartment,1971/72
- Mi-2 with special hang pod,experimental,1972
- Mi-2 Flying Crane was a flying crane version,powered by two GTD-350 turboshaft engines of 1973
- Mi-2R was a tactical photo reconnaissance version,powered by two GTD-350 turboshaft engines of 1970s
- Mi-2RO was a reconnaissance version equipped with cameras,powered by two GTD-350 turboshaft engines of 1970s
- Mi-2M2 was a variant of M1,with enlarge cargo cabin,up to 9 passenger,1974
- Mi-2KR was a reconnaissance and spotter version,1974
- Mi-2M Second use was a modernized version,built in Polish,with gas turbine
engines,1974
- Mi-2Ch/Mi-2CHR/Mi-2RHR was a chemical reconnaissance / smokescreen layer version
- Mi-2D was an Aerial command post equipped with R-111 radio
- Mi-2V was an export version to Libya,1970s
- Mi-2 Paltan was an Aerial minelayer version with 20 tube launchers on external pods and in left cab door, each for six or nine mines,1981
- Mi-2URS was anti-helicopter version,1982
- Mi-2URP-G was the Mi-2URP with additional 4x AA missiles Strzała-2 (Strela 2) in two Gad rocket launchers,also as Anti-helicopter version,1984
- Mi-2F Second use was an aerial photographic version
- Mi-2A was dual control and trainer version,with a modernized shape,powered
by two AI-450 engines,2003
- Mi-2B was an Upgraded export version for the Middle East, fitted with improved systems and navigational aids
- Mi-2V was a modernized version
- Mi-2G was also a modernized version
- Mi-2MSB or MSB-2 Nadia ('Hope') was a Modernized by Motor Sich to passenger-transport version for the civil aviation
- Mi-2MSB-V or MSB-2MO was a Modernized by Motor Sich for Ukrainian Air Force. Original engine replaced with AI-450M 465 hp (347 kW) engine, armed with rocket and machine gun pods, IR-jamming system and flares dispenser for defence against MANPADS
Mi-2

- To be continued

Mil Mi-2 - Wikipedia

en.wikipedia.org

 

[AM]

For Mi-2,

- V-2 was an experimental light helicopter and medium transport,powered
by two GTD-350 turboshaft engines,1960/61
- V-2 was an agricultural helicopter,powered by two GTD-350 turboshaft engines
of 1962
- V-2 was a transport helicopter project with 10 passenger,powered by two
GTD-350 turboshaft engines of 1964
- V-2M was a marine helicopter version,with emergency inflatable balloons,
powered by two GTD-350 turboshaft engines of 1965
- V-2V was an armament prototype,also powered by two GTD-350 turboshaft
engines
- Mi-2 was another combat helicopter,powered by two GTD-350 turboshaft
engines of 1965
- Mi-2T was a multi-purpose light helicopter,powered by two GTD-350 turboshaft engines of 1965
- Mi-2S was an ambulance version,powered by two GTD-350 turboshaft engines
of 1965
- Mi-2SR was also an ambulance and rescue version,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2Ch was an agricultural helicopter as a Polish version,powered by two
GTD-350 turboshaft engines of late 1960s

- To be continued

Mil Mi-2 - Wikipedia

en.wikipedia.org

 

[hesham]

For Mi-2,

- V-2 was an experimental light helicopter and medium transport,powered
by two GTD-350 turboshaft engines,1960/61
- V-2 was an agricultural helicopter,powered by two GTD-350 turboshaft engines
of 1962
- V-2 was a transport helicopter project with 10 passenger,powered by two
GTD-350 turboshaft engines of 1964
- V-2M was a marine helicopter version,with emergency inflatable balloons,
powered by two GTD-350 turboshaft engines of 1965
- V-2V was an armament prototype,also powered by two GTD-350 turboshaft
engines
- V-2 was a version ,with a comfortable salon,1967
- Mi-2 was another combat helicopter,powered by two GTD-350 turboshaft
engines of 1965
- Mi-2T was a multi-purpose light helicopter,powered by two GTD-350 turboshaft engines of 1965
- Mi-2S was an ambulance version,powered by two GTD-350 turboshaft engines
of 1965
- Mi-2SR was also an ambulance and rescue version,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2Ch was an agricultural helicopter as a Polish version,powered by two
GTD-350 turboshaft engines of late 1960s
- Mi-2P was a passenger and cargo version, with accommodation for 6 to 8 passengers,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2P Salon was a comfortable salon,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2Sh/Mi-2U/UMi-2/Mi-2SZ were a dual control trainer versions,powered by two GTD-350 turboshaft engines of late 1960s
- Mi-2M with a 4 bladed and enlarge fuselage,project of 1967,but powered
by two "GTD-550" turboshaft engines
- Mi-2M1 was a version with gas turbine,1968
- Mi-2RM was a sea rescue version equipped with electric winch for two people and dropped rafts,powered by two GTD-350 turboshaft engines of 1969
- Mi-2RL was a land rescue and ambulance version,powered by two GTD-350 turboshaft engines of 1969
- Mi-2F was a photographing and mapping version,powered by two GTD-350 turboshaft engines of 1969
- Mi-2FM was a survey version,powered by two GTD-350 turboshaft engines of 1969
- Mi-2 was a flying laboratory version,1971
- Mi-2US was an Armed version fitted with a fixed 23mm NS-23 cannon, 4 x 7,62mm PKT machine gun pods and optional cabin PK machine gun,1970/71
- Mi-2URN was an Armed variant with a fixed 23mm NS-23 gun and two 16x57mm S-5 unguided rocket pods Mars-2. Optional 7,62mm PK machine gun window-mounted,1971/72
- Mi-2URP was an Anti-tank variant, armed with 23mm NS-23 gun, optional window-mounted 7,62mm PK machine gun, and 4x AT-3 Sagger (9M14M Malutka) wire-guided missiles on external weapons racks and 4x additional missiles in the cargo compartment,1971/72
- Mi-2 with special hang pod,experimental,1972
- Mi-2 Flying Crane was a flying crane version,powered by two GTD-350 turboshaft engines of 1973
- Mi-2R was a tactical photo reconnaissance version,powered by two GTD-350 turboshaft engines of 1970s
- Mi-2RO was a reconnaissance version equipped with cameras,powered by two GTD-350 turboshaft engines of 1970s
- Mi-2M2 was a variant of M1,with enlarge cargo cabin,up to 9 passenger,1974
- Mi-2KR was a reconnaissance and spotter version,1974
- Mi-2M Second use was a modernized version,built in Polish,with gas turbine
engines,1974
- Mi-2Ch/Mi-2CHR/Mi-2RHR was a chemical reconnaissance / smokescreen layer version
- Mi-2D was an Aerial command post equipped with R-111 radio
- Mi-2V was an export version to Libya,1970s
- Mi-2 Paltan was an Aerial minelayer version with 20 tube launchers on external pods and in left cab door, each for six or nine mines,1981
- Mi-2URS was anti-helicopter version,1982
- Mi-2URP-G was the Mi-2URP with additional 4x AA missiles Strzała-2 (Strela 2) in two Gad rocket launchers,also as Anti-helicopter version,1984
- Mi-2F Second use was an aerial photographic version
- Mi-2A was dual control and trainer version,with a modernized shape,powered
by two AI-450 engines,2003
- Mi-2B was an Upgraded export version for the Middle East, fitted with improved systems and navigational aids
- Mi-2V was a modernized version
- Mi-2G was also a modernized version
- Mi-2MSB or MSB-2 Nadia ('Hope') was a Modernized by Motor Sich to passenger-transport version for the civil aviation
- Mi-2MSB-V or MSB-2MO was a Modernized by Motor Sich for Ukrainian Air Force. Original engine replaced with AI-450M 465 hp (347 kW) engine, armed with rocket and machine gun pods, IR-jamming system and flares dispenser for defence against MANPADS
Mi-2

- To be continued

Mil Mi-2 - Wikipedia

en.wikipedia.org

I complete the Mi-2 Variants.

 

[hesham]

For Mi-4,

- V-12 (First use of the designation) was a heavy transport helicopter project
of late 1940s,powered by one ASh-62 engine
- V-12 was a tandem twin rotor helicopter project of late 1940s,powered by
two ASh-62 engine
- VD-12 was a 12 seat carrying capacity with 57mm machine gun,experimental
helicopter of 1952,powered by one ASh-82V engine
- Mi-4 was a production version of VD-12,1953,powered by one ASh-82V
engine
- Mi-4GF was a factory designation for demilitarised Mi-4 for use in the Civil Air
Flee,powered by one ASh-82V engine,1953
- Mi-4PL or PLO was an Anti-submarine warfare helicopter,powered by one ASh-82V engine,1953
- Mi-4P & Mi-VP were a Civil transport helicopter, with accommodation for between 8 and 11 passengers, plus eight stretchers and a medical attendant
for air ambulance duties. It has square. windows compared to the circular
windows of the military versions,powered by one ASh-82V engine,1954
- Mi-4S was a VIP transport helicopter,powered by one ASh-82V engine,
1954
- Mi-4A or Mi-4VA was an Assault transport helicopter,powered by one ASh-82V engine,1954
- Mi-4Skh was a Multi-role agricultural helicopter, with a large chemical container in the main cabin. Also used as a fire-fighting helicopter,powered by one ASh-82V engine,1954
- Mi-4L was a Six-seat VIP transport version, sometimes converted into an air ambulance helicopter,powered by one ASh-82V engine,1954
- Mi-4VL was a Fire-fighting version of Mi-4L,powered by one ASh-82V engine,1954
- Mi-4AP was a Flying laboratory for testing autopilot,powered by one ASh-82V engine,1955
- Mi-4BT was a Minesweeper with floats helicopter,powered by one ASh-82V engine,1955
- Mi-4FV or Mi-4KV was a Photographic and guidance helicopter,powered by one ASh-82V engine,1955
- Mi-4Schch was a "Polar version" of Mi-4FV for working at the Soviet Arctic and Antarctic research stations,powered by one ASh-82V engine,1955
- Mi-4M was a medical version,powered by one ASh-82V engine,1956
- Mi-4SP was a version for Special rescue modification,powered by one ASh-82V engine,1956
- Mi-4PG was an Experimental version equipped with an external load sling
system,powered by one ASh-82V engine,1956
- Mi-4SV was a version with improved heat insulation for working in the
Far North,powered by one ASh-82V engine,1956
- Mi-4P was a 10-seat version with a seats from Il-18,powered by one ASh-82V engine,1957
- Mi-4S was a helicopter cabin,for Yemen government,powered by one ASh-82V engine,1957
- Mi-4ADT was a version with new blades with reinforced spar, increased stabilizer area, autopilot,powered by one ASh-82V engine,1957
- Mi-4A second use was a version with radio equipment "Prefix" or for
controlling automatic balloons,powered by one ASh-82V engine,1957
- Mi-4RI was a version of Mi-4M equipped with the Rion experimental sonar,
powered by one ASh-82V engine,1957
- Mi-4 was a version with the Pristavka (Add-on) radio equipment developed in 1957 for guidance of remote-controlled reconnaissance balloons,powered by one ASh-82V engine
- Mi-4AV was an Armed versions based on the Mi-4A. V for Vooruzhenniy
(Armed). Mi-4A with additional armament. Modification of 1967 had weapons complex K-4V, included four 9М17М ATGM "Phalanga" and 96 57-mm NAR
S-5M in six blocks UB-16-57U (or six 100-kg bombs or four 250-kg bombs
or tanks with an incendiary substance),powered by one ASh-82V engine,
1958
- Mi-4AV Second use was a transport and combat, with 2 TRS-132 blocks or 6 UB-16-57 blocks,powered by one ASh-82V engine,1958
- Mi-4N "Filin" (Horned owl) was an Experimental reconnaissance version intended for night-time use,powered by one ASh-82V engine,1958
- Mi-4SP or Mi-4PS was a Special rescue modification,powered by one ASh-82V engine,1958
- Mi-4VM (VM-12) was an Anti-submarine warfare helicopter,powered by one ASh-82V engine,1959
- Mi-4S Salon was a VIP transport helicopter,powered by one ASh-82V engine,1959
- Mi-4MR or Mi-4AM was an Upgraded version of Mi-4VM with the searching
radar station "Rubin-V" instead of "Kurs-M",powered by one ASh-82V engine,
1959
- Mi-4A Third use was an attack and assault helicopter,powered by one ASh-82V engine,1959
- Mi-4 was a version with in flight refueling system,powered by one ASh-82V engine,1960
- Mi-4A Fourth use was a modified for transporting and laying gas pipelines,powered by one ASh-82V engine,1961
- Mi-4KK or Mi-4VKP was a Mobile command post,powered by one ASh-82V engine,1961
- Mi-4KU or Mi-4VPU was a Mobile command post for controlling Air Force units,
powered by one ASh-82V engine,1961
- Mi-4U was a Target-designator version carrying the Oospekh (Success) system,
powered by one ASh-82V engine,1961
- Mi-4GR was a version with the wide-range panoramic radar detection,powered by one ASh-82V engine,1963
- Mi-4TARK was a version with TV-equipped artillery reconnaissance and spotting helicopter,powered by one ASh-82V engine,1963
- Mi-4MT was a Torpedo-carrying ASW attack (killer) aircraft derived from Mi-4M,
powered by one ASh-82V engine,1963
- Mi-4MU was an attack helicopter version,powered by one ASh-82V engine,
1963
- Mi-4MO was a search helicopter with Oka sonar,powered by one ASh-82V engine,1963
- Mi-4MS was a search helicopter with Soora infra-red sensor,powered by one ASh-82V engine,1963
- Mi-4ME was an Export version of the Mi-4M. With the RBP-4G search radar,
powered by one ASh-82V engine,1964
- Mi-4P Second use was a 13-passenger with autopilot version,powered by one ASh-82V engine,1964
- Mi-4MK or Mi-4PP was an ECM version,powered by one ASh-82V engine,
1964
- Mi-4 was a version with the Panorama circular filming equipment,powered by one ASh-82V engine,1965
- Mi-4AV Third use was a transport and combat, with 8 UB-16-57 blocks,powered by one ASh-82V engine,1965
- Mi-4AV Fourth use was a transport and combat, with the K-4V weapons
system (4 ATGM 9M17M, 8 UB-16-57 blocks),powered by one ASh-82V engine,1967
- Mi-4 was an anti-tank minelayer version,powered by one ASh-82V engine,
1967
- Mi-4 was a minelayer version produced by converting troop-carrier helicopters,
powered by one ASh-82V engine,1967
- Mi-4 was a flying laboratory with a device for detecting nuclear submarines by their radioactive trace,powered by one ASh-82V engine,1967
- Mi-4s was an agricultural helicopter version,powered by one ASh-82V
engine,1968
- Mi-4UM was a radio-controlled target drone version,powered by one ASh-82V
engine,1979
- Mi-4


- To be continued

Mil Mi-4 - Wikipedia

en.wikipedia.org

 

[hesham]

I finished the Mi-4 variants,and by the way,I add many many versions
don't mentioned in Wikipedia list,.

Great thanks to my dear AM.

 

[AM]

I finished the Mi-4 variants,and by the way,I add many many versions
don't mentioned in Wikipedia list,.

Great thanks to my dear AM.

Hi

Next part (Mi-6 and Mi-22)

 

[AM]

For Mi-4,

- V-12 (First use of the designation) was a heavy transport helicopter project
of late 1940s,powered by one ASh-62 turboshaft engine
...

ASh-62 and Ash-82 - pistone engines
MSB-2 Nadia ('Hope') - Nadia is a feminine name

 

[hesham]

Thank you my dear AM,and Nadia is also in Arabic Language.

*** For Mi-6,

- V-50 was a project of a heavy transport and assault helicopter with a gas turbine engine,1952,powered by one TV-2V engine
- VM-6 was a heavy transport project of 1952,powered by two TV-2V engines
- V-6 was a rotary wing project of 1953,powered by two TV-2V engines
- V-6 was a heavy helicopter project 1953,powered by two TV-2F engines
- Mi-6 was a heavy transport, experimental helicopter,with capacity of 150 seat, 2 ASU-57, 1 BTR-152 or 12 tons of cargo,two craft were built,and the 2nd with a wing, external suspension system, autopilot,powered by two TV-2VM engines,1957
- Mi-6 was an experimental, with trapezoidal blades,five were built,1959,powered
by two TV-2V engines
- Mi-6 was a version with rectangular blades,powered by two TV-2V engines,
1959
- Mi-6 was a transport version,maybe for civil use,powered by two TV-2V engines,1959
- Mi-6A was a military troop carrier,61 seat,powered by two TV-2V engines,
1959
- Mi-6S was an ambulance version,with 41 patients and 2 paramedic,powered by two TV-2V engines,1960
- Mi-6TZ or Mi-6ATZ was a fuel transport helicopter variant of the Mi-6A,powered by two TV-2V engines,1961
- Mi-6PR was an Electronic warfare version,with a protection of air defense radars from detection by reconnaissance,powered by two TV-2V engines,1962
- Mi-6 was developed in 1962 with collapsible BU-75BRM drilling rig for oil exploration in Siberia,powered by two TV-2V engines
- Mi-6PRTBV was a few modified as mobile missile maintenance technical bases and missile transporters,powered by two TV-2V engines,1962
- Mi-6 was a Missile fuel transport to supplement the Mi-6PRTBV,1960s
- Mi-6RVK was tested in 1965 loaded with 9K53, 9K73, 9M21 Luna-MV or 8K114 mobile missile systems,powered by two TV-2V engines
- Mi-6RVK Second use was also tested in 1965 loaded with 9K53, 9K73, 9M21 Luna-MV or 8K114 mobile missile system,powered by two TV-2V engines
- Mi-6M was an Anti-submarine variant armed with four aerial torpedoes and ASW rockets, and equipped with various experimental ASW systems. First built in 1963 and modified in 1965 for the "Barge Hauler" program,powered by two TV-2V engines
- Mi-6 was a passenger transport version,powered by two TV-2V engines,
1963
- Mi-6 was a tugboat of a sonar or mine trawl,powered by two TV-2V engines,
1965
- Mi-6P was a passenger transport helicopter, with accommodation for 80 passengers. One prototype was converted from a stock Mi-6,powered by two TV-2V engines,1965
- Mi-6PS was a search and rescue (SAR) helicopter developed in 1966 for pick-up of the landed Vostok and Soyuz space modules,powered by two TV-2V engines
- Mi-6PZh was a Fire fighting variant, with a 12,000 L (2,639.63 imp gal; 3,170.06 US gal) tank in the cabin and six 1,500 L (329.95 imp gal; 396.26 US gal) bags suspended from the fuselage,powered by two TV-2V engines,1967
- Mi-6L was a Flying laboratory variant with D-25VF engines used for flight improvements of the Mi-6 and testbed for the powerplant of the Mi-12,1969
- Mi-6VKP was a Command post transport helicopter to deploy comms and war room on the ground, not usable in flight,powered by two TV-2V engines,1969
- Mi-6PZh2 was a second firefighting helicopter prototype and several conversions with a steerable water cannon in the nose,powered by two TV-2A engines,1971
- Mi-6A Second use was a Troopships and commercial transport helicopters built to a new baseline standard with improvements in reliability and new avionics,powered by two TV-2V engines,1971
- Mi-6APS was a limited number of search and rescue helicopters converted
from Mi-6A,powered by two TV-2V engines,1970s
- Mi-6PSA was a search and rescue (for search and rescue of the Vostok and Soyuz type aircraft). Based on the Mi-6A,powered by two TV-2A engines,1973
- Mi-6ATZ was a Fuel transport helicopter variant of the Mi-6A,powered by two TV-2V engines,1973
- Mi-6 was a version with additional antennas on the fuselage and tail boom,
powered by two TV-2V engines,1974
- Mi-6R was a specialised radio communications relay variant developed in 1974, prototype conversions only,powered by two TV-2V engines
- Mi-6A VKP was an airborne command post) Command post transport helicopter to deploy comms and war room on the ground, not usable in flight,powered by two TV-2V engines,1974
- Mi-6AYA was the OKB designation for the Mi-6VzPU and Mi-22 airborne command posts, with SLAR,powered by two TV-2V engines,1975
- Mi-6VR was a water spraying research helicopter to test helicopter anti-icing systems,powered by two TV-2V engines,1976
- Mi-6 was an experimental conversion in 1976 for testing the rotor system of
the Mi-26,with 8 blades
- Mi-6PP was a prototype Counter-ELINT aircraft to protect air-defense radars from enemy ECM and/or ELINT activities,powered by two TV-2V engines,1980
- Mi-6M Second use was a projected redesign of the Mi-6 to carry 11 to 22 t (11,000 to 22,000 kg; 24,000 to 49,000 lb) over 800 km (500 mi), cancelled due to the limitations of the five-bladed rotor specified,powered by two TV-2V engines,
1980s
- Mi-6 Boorlak (boorlak – barge hauler) Prototype ASW/MCM helicopters, used for research into ASW equipment when delays to the mission equipment forced cancellation,19xx ?
- Mi-6T(NATO – Hook-A) Military transport helicopter, which can seat up to 70 people on tip-up-seat along the cabin sides, with additional seat along the center-line
- Mi-6TP was a convertible freight/passenger helicopter,19xx ?
- Mi-6TZ was a Fuel transport helicopter to refuel vehicles and helicopters on the ground,19xx ?
- Mi-6TZ-SV was a Fuel transport helicopter to refuel vehicles on the ground,
19xx ?
- Mi-6VUS (NATO – Hook-D) airborne command post with SLAR,19xx ?
- Mi-6VzPU (NATO – Hook-D) Service designation of the Mi-6AYa airborne command post with SLAR, entered service as the Mi-22
- Mi-6

- Mi-22VVS designation of the Mi-6AYa/VzPU airborne command post helicopters
- Mi-22/II was a 1965 Soviet project to develop a military transport helicopter,
it was a development of the Mi-2,powered by one 940 GTD-10A turboshaft
engine

- To be continued

Mil Mi-6 - Wikipedia

en.wikipedia.org

 

[hesham]

I complete also Mi-6 Variants.

 

[hesham]

For Mi-10,

- V-10 or Mi-10 was a heavy helicopter based on Mi-6,for transport
and cargo duties,had an external sling,powered by two D-25V
engines,1960
- Mi-10 was initial standard long-legged production helicopter,
powered by two D-25V engines,early 1960s
- Mi-10 was a series of production from 1964,powered by two D-25V
engines
- Mi-10R was a single standard production model fitted with a conventional undercarriage taken from the Mi-6 modified with spats and fairings, as well
as a twin wheeled tail bumper. Some Western sources erroneously cite this
aircraft as the Mi-10K,powered by two D-25V engines,1965
- Mi-10RVK was a Numerous variations of heliborne missile systems were envisaged, but only the 9K74 (aka S-5V) system reached the flight test stage. Missiles on launchers were carried complete with tractor units to be deployed on landing,powered by two D-25V engines,1965
- Mi-10K was a flying crane helicopter with short-legged narrow-track undercarriage and a ventral gondola for a second pilot,powered by two
D-25V engines,1966
- Mi-10GR was a single production Mi-10 fitted with Grebeshok (Comb) direction finding equipment, for ELINT (Electronic Intelligence) duties, in a pod slung between the undercarriage legs,powered by two D-25V engines,1966
- Mi-10UPL was a single prototype modified to carry a detachable mobile laboratory module for ore analysis,powered by two D-25V engines,1966
- Mi-10PP was an ECM (Electronic Counter-Measures) helicopter, preferred
military alternative designation,powered by two D-25V engines,1970
- Mi-10P was a Company / government designation for the ECM Mi-10PP,
powered by two D-25V engines,1970
- Mi-10 Flying Crane was a single prototype modified with 4,800 kW (6,500 hp) Soloviev D-25VF engines, new equipment and an up-rated transmission system,
,powered by two D-25V engines,1970
- Mi-10

Mil Mi-10 - Wikipedia

en.wikipedia.org

 

[AM]

For Mi-10,

- V-10 or Mi-10 was a heavy helicopter based on Mi-6,for transport
and cargo duties,had an external sling,powered by two D-25V
...

Hi

I draw your attention to the designations of the “izdelie” type. These are the designations of the Mil Design Bureau itself and it would be good to indicate them too

 

[hesham]

Thank you my dear AM,and I have more about Izdelie.

** For V-12,Mi-12;

- V-12 was a tandem rotor heavy transport helicopter,powered by four
D-25V turboshaft engines,project of 1959
- V-12 was a smaller version of above,also powered by four D-25V turboshaft
engines,project of 1959
- V-12 was another tandem rotor configuration helicopter,but powered
by two D-25V turboshaft engines, 1959 up to 1962
- V-12 was a large and heavy helicopter with single main rotor,also powered
by four D-25V turboshaft engines,project of 1962/63
- V-12 was a heavy helicopter with single main rotor,but powered by two
GTD turboshaft engines,project of 1963 to 1965
- V-12 was heavy transport helicopter,with two airscrew transverse rotors,
powered by four D-25VF turboshaft engines,1967
- V-12 or Mi-12M was a further proposed refinement of the V-16 with two
15,000 kW (20,000 hp) Soloviev D-30V (V - Vertolyotny - helicopter) turboshafts driving six bladed rotors, to transport 20,000 kg (44,000 lb) over 500 km (310 mi)
or 40,000 kg (88,000 lb) over 200 km (120 mi). The Mi-12M was cancelled at
the mock-up stage when the V-12 development programme was cancelled,
1966

- V-16 Early version was a project of a super-heavy crane helicopter,
early 1960s,could carry 40 to 50 ton,the version with a 3-rotor design,
powered by six D-25VF engines
- V-16 was a last version,with two air-screw transverse rotor,and powered
by two GTD engines

Mil V-12 - Wikipedia

en.wikipedia.org

Mil V-16 - Wikipedia

en.wikipedia.org

 

[hesham]

For Mi-14,

- V-8G or V-14 was anti-submarine helicopter project,in research and attack version,
powered by two Klimov TV2-117 engines,1959
- V-14 was a research and strike version,powered by two Klimov TV2-117 engines,
project 1966
- V-14 was also research and strike version,powered by two Klimov TV3-117M engines,project 1966
- V-14 was a prototype form of earlier,also powered by two Klimov TV2-117 engines,1967
- Mi-14 was an experimental helicopter,a converstion of Mi-8,powered by two Klimov TV3-117M engines,1970
- Mi-14PL was an Anti-submarine warfare helicopter, equipped with towed
APM-60 MAD, OKA-2 sonobuoys and a retractable Type 12-M search radar,
armed with either a single AT-1 or APR-2 torpedo, one Skat nuclear depth
bomb or eight depth charges,powered by two Klimov TV3-117M engines,1973
- Mi-14PL was an export version of Mi-14PL,powered by two Klimov TV3-117M engines,1977
- Mi-14BT was a mine sweeping helicopter with ASW systems removed
and equipped for towing Mine Countermeasures sleds. 25–30 built, with
six exported to East Germany and two to Bulgaria,powered by two Klimov TV3-117M engines,1979
- Mi-14PS was a search and rescue version with search lights and sliding doors with hoist,powered by two Klimov TV3-117M engines,1979
- Mi-14PLM was an improved anti-submarine warfare version with Os'minog
ASW suite, with new search radar, dipping sonar and digital computer. Limited
use,powered by two Klimov TV3-117M engines,1979
- Mi-14PL Second use was an experimental attack helicopter carrier of various types of anti-ship missiles,powered by two Klimov TV3-117M engines,1983
- Mi-14PS was a version with an ensure training landings,powered by two Klimov TV3-117M engines,1987
- Mi-14PS Second use was a version with laser-TV search system,powered by two Klimov TV3-117M engines,1987
- Mi-14PS Third use was a version with insulated cargo cabin,powered by two Klimov TV3-117M engines,1989
- Mi-14PS Fourth use was a rearch and rescue version with search lights and
sliding doors with hoist,powered by two Klimov TV3-117M engines,1989
- Mi-14PZh was an amphibious firebuster version of Mi-14BT. Conversion price about USD1M,powered by two Klimov TV3-117M engines,1993
- Mi-14GP was a conversion of Mi-14PL to 24–26 seat civil passenger transport,
powered by two Klimov TV3-117M engines,1995
- Mi-14PX was a search and rescue training helicopter for the Polish Navy (unofficial designation). One Polish Mi-14PŁ helicopter was temporarily
converted into the Mi-14PX, then converted back in 1996,powered by two
Klimov TV3-117M engines
- Mi-14PZh Second use was a version for firefighting, with an aviation complex
for extinguishing ground fires,powered by two Klimov TV3-117M engines,1999
- Mi-14R was a flying laboratory for testing the Ros-V OGAS and other weapons,
powered by two Klimov TV3-117M engines,2000s
- Mi-14PL/R was a Polish conversion of two Mi-14PŁ (Polish designation for Mi-14PL) to search and rescue version, with ASW equipment removed, developed
in 2010,
- Mi-14

- To be continued

Mil Mi-14 - Wikipedia

en.wikipedia.org

 

[hesham]

I finished the Mi-14 variants,and I add many versions,never mentioned in
the Wikipedia's site.

 

[hesham]

For Mi-20,

- Mi-20 was a five-seat project,1964. A version of the Mi-2 as amulti-
purpose light helicopter,with an extended fuselage and a gas turbine
engine,powered by one TVD-10 engine
- Mi-20 was a light multi-purpose helicopter project,1965. Mi-2 variant with
an extended fuselage,but powered by one GTD-350 engine
- Mi-20 was a project version,powered with American Continental T65 engine,1965
- Mi-20 was a [roject version, powered with a French Turbomeca Astazou - XIV
engine 1965 up to 1976
- Mi-20 was a project version,but powered by one GTD-550 engine,late
of 1960s
- Mi-20 was a four-seat project version,but powered by one GTD-11 ENGINE,
1972
- Mi-20

Mil Mi-20 - Wikipedia

en.wikipedia.org

https://www.secretprojects.co.uk/threads/mil-mi-20-project-of-1966.10872/

 

[hesham]

Thank you my dear AM,and I have more about Izdelie.

** For V-12,Mi-12;

- V-12 was a tandem rotor heavy transport helicopter,powered by four
D-25V turboshaft engines,project of 1959
- V-12 was a smaller version of above,also powered by four D-25V turboshaft
engines,project of 1959
- V-12 was another tandem rotor configuration helicopter,but powered
by two D-25V turboshaft engines, 1959 up to 1962
- V-12 was a large and heavy helicopter with single main rotor,also powered
by four D-25V turboshaft engines,project of 1962/63
- V-12 was a heavy helicopter with single main rotor,but powered by two
GTD turboshaft engines,project of 1963 to 1965
- V-12 was heavy transport helicopter,with two airscrew transverse rotors,
powered by four D-25VF turboshaft engines,1967
- V-12 or Mi-12M was a further proposed refinement of the V-16 with two
15,000 kW (20,000 hp) Soloviev D-30V (V - Vertolyotny - helicopter) turboshafts driving six bladed rotors, to transport 20,000 kg (44,000 lb) over 500 km (310 mi)
or 40,000 kg (88,000 lb) over 200 km (120 mi). The Mi-12M was cancelled at
the mock-up stage when the V-12 development programme was cancelled,
1966

- V-16 Early version was a project of a super-heavy crane helicopter,
early 1960s,could carry 40 to 50 ton,the version with a 3-rotor design,
powered by six D-25VF engines
- V-16 was a last version,with two air-screw transverse rotor,and powered
by two GTD engines

Mil V-12 - Wikipedia

en.wikipedia.org

Mil V-16 - Wikipedia

en.wikipedia.org

I add V-16 to V-12 variants.

 

[igor-mich]

V-37(Mi-37)

 

[hesham]

For Mi-24,

- V-24 was utility and attack helicopter project of 1966,looks like Bell UH-1A,
and powered by one TV3-117 engine
- V-24 was another project,very close to the final form,but powered by tw5
TV3-117 engines,1967
- Mi-24 was experimental transport and attacke helicopter,with more capacity
to carry weapons,powered by two TV3-117 engines,1969
- Mi-24 was also experimental transport and attack helicopter,with a refine
shape,powered by two TV3-117 engines,1970,
- Mi-24A was a production version,powered by two TV2-117 engine,it
was appeared in 1971/72
- Mi-24B was an experimental variant of the Hind-A, one of which was used
to test the Fenestron tail rotor,powered by two TV3-117 engines,1971
- Mi-24U wasa training version without nose gun and wingtip stations,1972
- Mi-24A/II was the second production model. Both the Mi-24 and Mi-24A entered into Soviet Air Forces service in 1972. It lacked the four-barrel Yak-B 12.7mm machine gun under the nose
- Mi-24V was a aversion with tandem cabin,and USPU-24 machine gun,powered
by two TV3-117 engines,1972
- Mi-24V was a (Hind-E) later development which entered production in 1976.
It was armed with the more advanced 9M114 Shturm (AT-6 Spiral). Eight of
these missiles are mounted on four outer wing pylons,1976
- Mi-35 (Mi-35V) was exported version of Mi-24V,powered by two TV3-117V
engines,1970s
- Mi-24M was an anti-submarine project version,powered by two TV3-117
engines,1970
- Mi-24BMT was a small number of Mi-24s converted into minesweepers,
powered by two TV3-117 engines,1973
- Mi-24D (Hind-D) The Mi-24D was designed to be a more pure gunship than the earlier variants. It entered production in 1973. The Mi-24D has a redesigned forward fuselage, with two separate cockpits for the pilot and gunner. It is armed with a single 12.7mm four-barrel Yak-B machine-gun under the nose. It can also carry four 57mm rocket pods, four SACLOS 9M17 Phalanga anti-tank missiles (a significant enhancement compared to the MCLOS system found on the Mi-24A), plus bombs and other weapons
- Mi-25 was an export version of the Mi-24D,powered by two TV3-117 engines
- Mi-24P (Hind-F) The gunship version, which replaced the 12.7mm machine-gun with a fixed side-mounted 30mm GSh-30-2K twin-barrel autocannon. Entered production in 1981
- Mi-24P was an exported version of Mi-24P,powered by two TV3-117V engines
- Mi-35P was also an exported version of Mi-24P,
powered by two TV3-117V engines,1975
- Mi-24 was an experimental version of Mi-24A,with a Fenestron tail rotor,powered
by two TV3-117 engines,1975
- Mi-24/A-10 was a designation given to the aircraft used for record breaking from 1975 in the FAI E1 class
- Mi-24R (Mi-24HR) was a radiation, chemical and bacteriological reconnaissance,
powered by two TV3-117V engines,1978
- Mi-24RR was a radiation reconnaissance model derived from the Mi-24R
- Mi-24K (Mi-24RK) (Hind-G2) was an army reconnaissance, artillery observation helicopter,powered by two TV3-117V engines,1978
- Mi-24DU was a small number of Mi-24Ds were built as training helicopters with doubled controls,powered by two TV3-117 engine,1980
- Mi-25U was exported version of Mi-24DU,also powered by two TV3-117
engines,1980
- Mi-24TECh-24 was an experimental Mi-24P to test abilities for recovery of downed aircraft,powered by two TV3-117 engines,1981
- Mi-24V was a flying laboratory for testing PrPNK-28 helicopter Mi-28,powered
by two TV3-117V engines,1982
- Mi-24VD was an experimental, with a rear turret with a NSVT-12.7 machine gun,
powered by two TV3-117V engines,1985
- Mi-24VP (Hind-E Mod) Development of Mi-24V made in 1985 which replaced the machine-gun with GSh-23 in a movable turret. Entered service in 1989
- Mi-24RA (Hind-G1 Mod) New version of the Mi-24V,powered by two TV3-117V engines,1989
- Mi-24VM was an upgraded Mi-24V with updated avionics to improve night-time operation, new communications gear, shorter and lighter wings, and updated weapon systems to include support for the 9M120 Ataka and Shturm ATGMs, 9K38 Igla [Air-to-air missile AAMs] and a 23mm main gun. Other internal changes have been made to increase the aircraft life-cycle and ease maintenance,powered by
two TV3-117VMA engines,1995
- Mi-35M was an exported version of Mi-24VM,powered by two TV3-117VMA engines,1995
- Mi-35M1 was an export version of Mi-35M, with non-retractable landing gear, increased stock of ASO-2V IR decoys (in two fairings with 3 cassettes with 32 rounds each), SPO-15 "Bereza" station, L-116V-11E active IR jamming station. Empty weight –8350 kg,powered by two TV3-117VMA engines,1995
- Mi-35M2 was an updated version of the Mi-35M for the Venezuelan Army,
powered by two TV3-117VMA engines,1995
- Mi-35M3 was an export variant of the Mi-24VM,powered by two TV3-117VMA engines,1999
- Mi-35M4 was an (AH-2 Sabre) Updated version of the Mi-35M,powered by two TV3-117VMA engines,2000s
- Mi-24PS was a civil police or paramilitary version, equipped with a FLIR, searchlight, loudspeaker PA system and attachments for rappelling ropes,
powered by two TV3-117VMA engines,1995
- Mi-24PN (Mi-35PN) (Hind-E) A night-attack version based on an Mi-24V in Mi-24VM Stage 1 configuration,powered by two TV3-117VMA-SBZ engines,2002
- Mi-24VK-1 (Mi-35VN) was a modernization option, with a 24-hour weapons system 9K113K, OPS-24N (GOES-342 with thermal imaging, TV, IR channels and laser), NPPU-23,powered by two VK-2500 engines,2002
- Mi-24VK-2 (Mi-35VN) was a modernization option: with a 24-hour weapons system 9K113K, OPS-24N (GOES-342 with thermal imaging, TV, IR channels and laser), NPPU-23,powered by two VK-2500 engines,2002
- Mi-24M was a modernized version of Mi-24D,powered by two VK-2500 engines,
2002
- Mi-35M was a modernization option: with a 24-hour weapons system 9K113K, OPS-24N, NPPU-24, ATGM "Ataka-V", X-shaped RV,powered by two VK-2500 engines,2003
- Mi-35M was intended for the Russian Air Force. OPS-24N with GOES-342, 23-
mm gun GSh-23L, (NPPU-23) ATGM "Shturm" ("Attack"). Prototype, 1 vehicle (tail number 50 - converted Mi-24VP),powered by two VK-2500-2 engines,2011
- Mi-24F (Hind-A) Modified Hind-A with seven reinforcing ribs on the port fuselage aft of the wing and the SRO-2M Khrom ("Odd Rods") IFF antenna relocated from the canopy to the oil cooler. The APU exhaust was also extended and angled downwards. The designation may be unofficial
- Mi-24PTRK was a modification of the Mi-24D that was used for testing the Shturm V missile system for the Mi-24V
- Mi-24VU (Hind-E) Indian training version of Mi-24V
- Mi-24PM was an upgraded Mi-24P using same technologies as in Mi-24VM. Currently delivered to the RuAF
- Mi-24 SuperHind Mk.II Modern western avionics upgrade produced by South African company Advanced Technologies and Engineering (ATE). Prototypes converted from Mi-24R models, and one Mi-24P was used to test sighting system
- Mi-24 SuperHind Mk.III Extensive operational upgrade of the original Mi-24 including weapons, avionics and counter measures.
- Mi-24 SuperHind Mk.IV Upgraded Mk. III version with Pall vortex engine air particle separator system over the engine intakes
- Mi-24 SuperHind Mk.V Newest version of the "SuperHind" with fully redesigned front fuselage and cockpit. Mock-up only
- Mi-24P-1M Latest modernization of Mi-24P helicopters, fitted with a new modular direct infrared countermeasures system, autopilot, improved power supply unit and OPS-24N-1L navigation and targeting station. It has also an option for an active electronically scanned array (AESA) radar. First unveiled at 2019 MAKS International Aviation and Space Salon
- Mi-35MS Flying Command Post variant of the Mi-35M. Operated by the Russian Federal Protective Service (FSO)
- Mi-35 Phoenix Russian Helicopters holding has developed a common standard for Mi-24 modernization designated as Mi-35P. The Mi-35P has received the OPS-24N-1L observation-sight system with a third generation long-wave matrix thermal imager, TV camera, and laser rangefinder. The upgraded gunship’s cockpit has the KNEI-24E-1 flight navigation system with multifunctional displays. The PKV-8-35 digital flight system increases the helicopter’s manoeuvrability and steadiness. The modernised gunship is also fitted with the updated PrVK-24-2 targeting system, which allows the use of 9M127-1 Ataka-VM anti-tank guided missiles and either L370 Vitebsk electronic countermeasure system or its export version President-S.The helicopter has also received a chin-mounted NPPU-23 turret with a twin-barrel GSh-23L autocannon.Serial production has started as of August 2020 for an export customer. It is also known under nickname Phoenix
- Mi-35U was an unarmed training version of the Mi-35

- To be continued

From Wikipedai and some books,

List of Mil Mi-24 variants - Wikipedia

en.wikipedia.org

 

[hesham]

I complete Mi-24 list with its variants.