Category Helicopters

W-3 Sokol

• Twin-turboshaft transport helicopter • Exports • Multi-role

Подпись: A PZL bogan its helicopter manufacture m the 1950s. Itconso-building Soviet Mil designs. Today tho company designs its own aircraft and sells them around the world.W-3 SokolIn 1979, with nearly 20 years’ experience of building Mil-designed hclicoptors behind it, Poland’s PZL Swidnik flew the first prototype of a new design designated W-3 and named Sok6l, or ’Falcon’. There was a long series of tethered tests and extensive design changes before the second prototypo flew in May 1982, and it was another three years before production began. Since then, PZL has developed several specialised variants for military and civil applications.

Frank Piasecki’s ‘flying banana’

S

ccin. ll ІІ1С Н-2Г6 potcntijl. (ІИ-* I >S Army awarded I’iasoik) a production оu iiract in 1952. H-21* bad estensive armour atxl the ability to cany two external fuel tanks, and Intn. KJuccd a 2-tonne hook.

In 1955. In the time lielio’pter pioneer Prank I’l. isecki was forced оШ ol tltc linn which Ixmr Іііч name (the ciHiipany becatlk* Vetiol. latei O’ ving-VVrtOl). the I S Army was the bluest user ol tills tandem, twin-rotor helicopter.

Ihe H-21 was l>a. sed on the t s ‘av> > IIKI’-i. ilsell a

Model 44A

Vertol produced a small number of Model 44s. which originated as the Piasecki PO-22. a civil version of the Workhorse. Belgium’s flag carrier SABENA operated a single leased example during the 1958 World Fair.

Accommodation: plot. co-piot. crew chef, and (to Vietnam) two gunners tor door-mountod

12.7- mm М2 or 7.62-mm M60 machine-guns, plus 20 troops or 12 stretchers

Dimensions:

mam rotor Олmeter 13.41 m (44 nj

tuselago length 18 m (52 ft. 6 in,)

height 4 8 m (15 ft. 9 in)

rotor disc area 282.52 m’ (3,0*1 sg. tt.)

COMBAT DATA

STRETCHERS

l-aUVUii

Kl traoo o> ІІЮ) 1)00* used Mngl* i*xai pwton engines. irvi Wright Cycione in me M-21 tuivng tn power two rmtn rotors the Skonfcy H 34 end н-to wee conventonal eng» men uxor dusa>a the former nav/vj the moil oov/<yJ engne UltxmMy turbonlialt ena-nos retraced rattele n most isrtcoorers.« mey are ughto end more powerte then e futon ongme оI lerslar wohjht.

И-34Л CHOCTAW IlMkW 1528 hp

Frank Piasecki’s ‘flying banana’

Frank Piasecki’s ‘flying banana’
Frank Piasecki’s ‘flying banana’

■ MODEL 1CH-1A PATHFINDER II: A joint ArmyVNavy funded programme to research compound helicopter designs led to the Pathfinder and Pathfinder II of the early – 1900s.

 

■ MODEL PV-15/H-18 TRANSPORTER: At

the time of its inception, the H-16 was the world’s largest horopter Flown In 1953. it was iudgcd unsuitable by tho OS Army

 

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НИ* CHOCTAW

 

!M к*Л |1П « »Х|

 

IOUCIUUW ІІвктк(і(2е« к |

 

Frank Piasecki’s ‘flying banana’

PZL Swidnik

H-21

• Transport helicopter • USAF’s first twin rotor • Vietnam action

Подпись: A Frank Piasccki's H-21/HRP made use of tho designer s well-known tandem rotor layout, perpetuated in the later Vcriol H-25JHUP. H-46 агні H-47 designs.Подпись: IH-21Developed for tho USAF from tho HRP tandem-rotor designs, the H-21 made Its mark with tho US Army, which named its the Shawnee. After missing the Korean War by just a year, the twin-rotor H-21 Workhorse (its USAF name) entered service with Army aviation units In the 1950s and went to war briefly In Vietnam in the 1960s, the swansong of its career. A few oxamples served with foreign forces, mainly under the Military Assistance Program.

▼ Shawnee in Vietnam

Подпись:Подпись:H-21Operated by tho Bth and 57th Transportation Companies, and armed with Browning machino-guns. tho CH-21C served (or just two years.

A Gallic ‘flying banana*

Delivered in 1957. French army H-21Cs saw service during the conflict in Algeria.

 

Border-to-border flight ►

An Army H-21 Shawnee became tho first helicopter to fly non-stop from tho US west coast to the cast coast On the way it was refuelled by a de Havilland Canada U- 1A Otter via a rudimentary hose system.

 

H-21

FACTS AND FIGURES

>• A fow examples of tho civil Plaseckl PD-22 (Vcrtol 44) servod with Now York Alrlinos and other carriors.

► Two H-21 Cs were re-engined with turboshaft», as XH-21Dn.

► Forolgn H-21 operators Included West Germany, Franco and Canada.

► Four US aviators klllod in nn H-21 In Jufy 1962 are recognised by some sources «» tho first American fatalities In Vietnam.

► The YH-21 prototypo for this series made

Its mnidon flight on 11 April 1952.

>• A total of 334 of those helicopters was produced for tho Unltod States Army.

Подпись: development of the fabric covered HKIM. Piaseeki s hrst successful tandem tutor design Over 100 H-21s were і ні ill for the Army, mostly of the H-21C variant. One of these made the first non-stop helicopter flight Irotn one coast of the US to the Other, refuelled aloft by a de I l.ivilkind I IA OUcr 11-2 Is arrived in VieUtam in December 1961, during the early iby* ol the l s build up H-21.% were exported under MAP, and a civil version the .Model И. ч.і\ limited scivitv with the Swedish IUIVA Подпись:Подпись:Подпись:Подпись:Подпись:Подпись:Подпись:H-21Подпись: Type: troopfeargo tandem rotor transport hsKooterПодпись:Подпись:Подпись:Подпись:Подпись: Weights: ompty 4060 kg (8,960 to ), maximum take-off 6895 xg (15.200 <X> >H-21Подпись: illis il 'ilH-21

Twin-rotor US Navy rescuer

D

esigned to meet д Naxy піхчі Гог л nhiplxwtd utility ln lU opiiT. Hr – Pfcuecki Model I’V-IH, known in naval parlance

.is tli. ІІП* Kemevei. Iir>i llew in l‘> and entered 4-nice thnx – vi ns Liter. Primitive by todays st. mil. mls. the III I* was ||ie finest ІК’ІІІМркТ III Its i|.«vs in tile 1‘Я0> It also чтмчі in the t*S Липу as the II-2S Army Mule With a single engine driving twin rotont and with its ГипсііошІ Inn odd-looking tail draper landing gear, the HI JT

и* Huo паз capacity w a crew or two and oitner kx« pu’-sengor» or throe stretch*» cases. An r, tornaSy-oporated «ьсиа lotcn rest to the preti soot was targe enough to aorornmoctote a toartod stretcher A Itydrocdc host above •hi – паеh was used 10 Mt scxvrvo* aboard wrue hovering

Above: Several US Navy HUP-2s had dunking sonar lilted for anti-submarlno operations and were designated HUP-2S.

HUP-2 Retriever

Thits HUP-2 сипім the markings ot Navy Utility
Helicopter Squadron 1. This unit operated
search-and-rescuo HUPs from various aircraft-
carriers during the Korean War.

US Navy carrier ‘planeguards*

 

■ SIKORSKY SH-3 SEA KING: Purchased m large numbers by the Navy, the SH-3 has served for more than 30 years Irom 1961.

Twin-rotor US Navy rescuer

 

■ SIKORSKY H04S: This naval version ot the SfrooAy S-55 was pnmanty an anti-submarine lion type, entering service in 19S0.

 

■ SIKORSKY HSS SEABAT: Delivered in 1955. tho first SrMbats replaced the HO-tS, which was short on range and load-capacity,

 

Twin-rotor US Navy rescuerTwin-rotor US Navy rescuer

Подпись: Below: Retnavers also served with the Marine Corps in transport and rescue roles from shore bases. The HUP was redesignated UH-25 in 1962.Twin-rotor US Navy rescuer

HUP-3 Retriever

Type: singlo-engmed. twin-rotor utility, cargo and rescue helicopter

Powerplant: one 410-KW |550hp l Comment»! R-9/5-46A radial eng**

Maiimum speed: 169 km*» (tos m p. h.)

Maximum range: 547 *>m (340 m p h.)

Service ceiling: .1050 m no.000 It)

Weights: empty 1782 kg (3.930 lb). maximum take-o»t 2767 kg (6.100 lb |

Accommodation: pilot, co-pilot and up to five

passengers or three hoepctal stretchers with attendant

Dimensions:

main rotor diameter 10.67 m (35 ft.)

fuselage length 17.3&m (57 ft I

height 3.81 m (12 ft. 6 in)

rotor disc area 178.76 пт1 (1.024 sq. ft.)

 

the twn rotor layout woe a trademark ot Prank N Rasedufc helicopter designs. T>*s layoul was

later ччггісі end BoenQ-VtMloi Onftgria and СИ-47 Chnook

 

ACTION DATA

 

Twin-rotor US Navy rescuer
Twin-rotor US Navy rescuer
Twin-rotor US Navy rescuer

Vxlngnt t***’ waa It* nomo gtwen to thm dark rmao лгксп ал»пга akhost a» US Млу a reran n mo 1950o.

 

■ SIKORSKY SH-60F SEAHAWK: The

carrier-borne version ol the SH-608. the F – model has a less comprehensive ASW suite

Twin-rotor US Navy rescuer

 

HWf-2 RETRIEVER

2 Ufa • 41

 

OtUOONFlT HR MX 1 2 став • 2 passcegeri

 

mmm

 

MO-2

t ««■ . I Mantra

 

Twin-rotor US Navy rescuerTwin-rotor US Navy rescuer

Piasecki/Vertol

HUP Retriever

• Single-engined, twin-rotor • ‘Planeguard’ • Utility helicopter

О no of the first helicopters to serve aboard US Navy warships, the HUP Retriever was one of several tandem, twin-rotor helicopters designed by rotary-wing pioneer Frank Piasccki in tho late-1940s and 1950s. Intended primarily for shore duty as a cargo hauler (in which rolo it also flew with the US Army), it is best remembered for its naval service and for rescuing many pilots who might otherwise have been lost at sea.

Piasecki HUP Retriever

HUP Retriever
Подпись:Подпись:HUP Retriever

la Canadian colours with VH-21 ►

The Royal Canadian Navy roceived three HUP-3s from the US Navy which wore operated by squadron VH-21. These wero among 50 ex-US Army H-25As transferred as surplus to the Navy.

FACTS AND FIGURES

> Tho Piasecki Aircraft Corp. of Morton, Pennsylvania, evolvod Into today’s Booing Helicopter Company.

> Tho first US Navy HUPs wore delivered to squadron HU-2 In Fobruary 1951.

> A Rotriovor could hovor at 15 m (50 ft.) and lift an airman weighing 75 kg (165 lb.).

>■ After being transferred to reserve units, some HUPS were retained as rescuo aircraft with an orange colour scheme.

► PV-18 production totalled 339, including 70 H-25s for tho US Army.

► Tho Army’s H-25s wore procured by the USAF on the Army’s behalf.

Подпись:HUP RetrieverПодпись:Подпись:HUP Retriever

NH 90

• European partners • Advanced design • Utility helicopter

The NH 90 project began in 1985 as a co-oporative projoct between European helicopter manufacturers for ‘a NATO helicopter for the 1990s’. Today, the NH 90 partner nations – France, Italy. Germany and the Netherlands – operate a mix of helicopters as battlefield transports and shipboard ASW aircraft. Because of dolays, the NH 90 is not now expected to ontor service until 2003, with the first dolivorics going to tho Netherlands navy.

NH 90NH 90▼ Difficult start

Britain was ono of the original parinors. but dockiod to drop out of tho protect at an early stage, in 1987.

▲ Future perfect

To help promote tho aircraft various artists’ impressions ol tho NH 90 were distributed to the aviation press.

◄ Military mock-up

Future military customers wen shown full-scale models ol the NH 90 to illustrate the potential of the design. This example war. displayed at Farnborough

◄ Shipboard warrior

Most European clients are intorostod In replacing their ageing Sea King fleet with a specialised variant of the NH 90. This version will be equipped with anti-ship missiles and torpedoes.

Future saviour ►

NH Industries has boon quick to see tho potential of tho NH 90 as a rescue helicopter. Civilian operators have shown interest in tho helicopter, although no orders havo been forthcoming.

Подпись: FACTS AND FIGURES ►

> Five European nations signod tho memorandum In 1985 allowing the dovelopmont of tho NH 90.

>• Two main vorsions (transport and naval) of tho NH 90 are being developed.

► Tho naval vorslon of the holicoptor will bo oqulpped with a search radar.

The work is being shared by Eurocopter
France (43%). Agusta (26%). Eurocoptor
Germany (24%) and Fokker (7%).

► Production of tho NH 90 is oxpoctod to

commence In 1999.

► The TTH version Is oxpoctod to cost FF90 million; the NFH FF145 million.

NH Industries NH 90

 

NH 90

NH 90 (provisional)

Type: transporVASW hodcoptw

Powerplant: two 1589.5-KW (2,145-hp.) Rol Royco/TurtoomOcarMTU RTM 322-01/9 turboshalt engines

Maximum speed: 295 krrvh (183 m. ph,)

Endurance: 5 hr 30 min

Combat radius: niO km (688 mt. j

Hovering celling: 3500 m 1З.500 n)

Weights: empty 5700 kg (12.540 lb,): maximum tako-oft 9Ю0 kg (20.020 lb)

Accommodation: three crow and 20 fully equipped troops

Dimensions:

main rotor diameter 16.30 m (53 ft. 6 in)

length 18.81 m (55 ft. 2 in.)

5.42 m (17 ft. 9 in I 713 82 m’ (2.300 sq M l

 

Below: The Hying prototype of the NH 90 has exceeded all the performance levels required for the design. Pilots have praised the he/rcopfer’s handling.

 

Italian Sea Kings and Ajtiwa-Bcll 212s. So far. (і Г NH 90s liavt* been ordered: the biggest customer is Italy, with 22 I examples The first рігкіїктіол example of the N11 90 Hew in May 200 )

 

mam rotor disc

 

NH 90

Tho tour-outdoe tad rotor e of compcc. ro construction otto rotates an 1235.4 tom The Mtote ta« pylon can too tor stcraj» on the NFH verson

 

I ho titanium man rotor hub Supports me »№/ composed bJuPM when htf. n aAranced aerofoils and curved tips lo reduce Рік}. Tfic WH verson wl nave automatic taking oi ttw man Wades

 

Thn NFH umion wij П0птаП> deny з Hqhi crow 01 tirw comjyoog u plot, a co-pW una one system operetor n the cabin.

 

NH 90

For rranrmo eperaton* tea Sea King ibeMwl ha» boon a commlcoo <У Western force» A apecUtocd variant at Яш NH 90 n m the process ot bong drrrttoooa to replace the agernj Son King m aorwoo ItaTy. Getmany and Fiance navu requeued я •,MVT equipped Wim a 360’ *e*rrh roifcjr nnd hjrapohts for arm – *ho mnrales and depth chargee The new helcopler was diwqritvi Horn mn outset to on abte to operate tram omul warshot toch as bigatos and doairoye»*

 

Mttdo by a European oensortum ol Turbomecrc Rote HoyOo, MtlJ, Piaggto and Tcpps. tho Iwn RTM 322 01/9 engnr» aie expK. fed to ася*л« nflw ktwta of rekoWUy.

 

NH 90 PT2

 

PT2 is pnintod in naval-stylo light grey camouflage and is ol basic configuration. As the second prototypo to (ly. on 19 March 1997. it also bocamo tho first example to operate with tly-by-wiro controls.

 

Tho – NH эоь fuselage is ccnstmclod n thtee count ner. The ticni tuseage <i buC at Mangnerve. France: the centre at Qttobmnr Germany, tne rear at Case па Co3ta. Italy.

 

Theta

 

to omr ts retractable and consists ot ti twrvwbor* nose unt and ■set man unis Emergency floatation gnar wtf attо bo available

 

European rotorcraft projects

 

■ EH INDUSTRIES EH101: This Angto-ltalmn ты*. . >rjt® helicopter has been ordered by Italy Hgihe UK. and Is being ottered (or export

 

■ EUROCOPTER TIGRE: Designed as an anti-tank and ground-support helicopter, the Tlgro has orders tor around 400 examples.

 

I EUROFAR : ManutiKturers trorn Franco, Germany and tne UK are examining the possibility of building this twin-eogindd tilt-rotor aircraft.

 

■ EUROCOPTER EC 135: This seven – or e=gM-80iit. light, turbine-powered aircraft is projected to have achieved 700 sales by 2007.

NH 90

 

NH 90NH 90NH 90NH 90NH 90

PlASECKI

Ml-34 ‘Hermit’

• Military trainer • Aerobatic • Liaison aircraft

First flown in 1986. the Mi-34 was designed as a replacement for the Mi-1 and Mi-2 helicopter trainers. It was also offered for the observation, liaison and border patrol roles. The Mi-34 can carry a maximum payload of 165 kilogrammos (360 lb.) of fuel over a distance of 160 kilometres (100 miles) and it fuel consumption is a modest 45 litres (12 gallons) per hour. A twin-engine version, flown for the first time iin 1993. has two VAZ-430 twin-chamber rotary engines.

Ml-34 ‘Hermit’
A Pilot trainer

Подпись:Ml-34 ‘Hermit’A military training variant has undergone flight testing with the Soviot armed forces as a possible replacement for the Mi – UMi-2.

◄ Flight performance

One of the latest helicopters developed in Russia, the •Hermit’ is sparsely equipped compared to its Western counterparts.

FACTS AND

>- Tho Mi-34 ‘Hermit’ was designed as a replacement Гог tho Mi-l/Mi-2 civil light helicopter and military trainor.

► ‘Hermit’ is tho first Soviet holicopter capable of executing a loop.

► Composite materials are used for the main rotor and tail blades.

FIGURES

> Mil first flow the Mi-34 ‘Hermit’

in 1986, using unboosted mechanical Right controls.

> A twin-engine version is built by the VAZ mole*

car works at Togliatigrad.

> The Mi-34VAZ features a totally now rotor head made from carbon fibre.

PROFIL

 

Ml-34 ‘Hermit’

Mi-34 ‘Hermit’

Type: фМ nWitary tramerfliaeon helicopter

Powerplant: one 242.5-kW (325-hp.) VMKB M – 14V-28 nine-cy^nder шг-cooled radial eng. ne

Maximum speed: ?10 krrvh (130 m p h)

Cruising speed: 180 km/h <112 m p h Range: :50 km (280 mi.)

Hover ceiling: 1500 m (4.920 ft.)

Weight: Normal take-off 1080 kg (2.380 1Ы Accommodation: :«vo pitots and two passengers Dimensions:

Span 10 m <39 ft 7 in.)

Length 11.4m (37 ft. 5 in,)

Height 2.8 m (9 tt. 2 in)

Main rotor area 78.54 m’ (845 *q tt.)

 

Left: After years of building military helicopters, the Ш design team is shifting its focus to the civilian helicopter market with the Mi-34

 

The twin engine Mi-.WAZ b built by the / automobile factory It lets a new rotor head fot enlunoeil control response, along with ііпрпл ed range, enilur. true and performance

 

Above: The Mt-34 haas stunned airshow audiences with its flight demonstrations. An example is seen here about to enter a loop.

 

ACTION DATA

 

latter 4«r»ons of the ‘hermit’ have two engnes ana ode» ncreased rarvjs and speed.

 

Th# Herml’ rue а емг щиО than ns Wruarn eouvatants marty boccause 0* >s rewtrvery poor quatty «ngino For «Пае» speed АіЧомміїаі»-» Gari-ln is in# lastost hotcootcv in its cbm

 

Compoorte structures are used mrouyou! the hbteoptor. particularly m the man and ini rotor sections This has ‘ixii/ced the Overat weight and трглей the safety ot the design Future MJ products wfl use more ccmxste ccmpcrees.

 

Seating * crovdod lor two ptktta. ttw mar of Ifw oockpt o devoted to cargo <* ми ■» xioonai two passengers Ftajht conlrob am inboontod mechaivcai ctrKrots imuring heavy nputs from the w*ot during си» turn manoeuvre*

 

Ml-34 ‘Hermit’

ишмсшш

 

1)0 ka. fi (t««i. pA.|

 

1ИкпЪ

(Itsaa-M

 

HOVER CEILING

 

МИЛИЦИЯ

 

Ml-34 ‘Hermit’

опасно

 

Ml-34 ‘Hermit’

AH ci/rent production Hermts’ have landing ste». attnough I he* design can bo equipped with wheels і needed

 

Multiple Mils

 

■ Mi-6 HOOK’: Fust of the heavywe-ght hehcopters m service, the Hoc*’ first tew in 1857 and remains *t front-line service.

 

■ Mt-17 •HIP’: Developed from me earl** Mt-8 in an effort to offrn improved performance, the МИ 7 паз seen widespread civtkm service.

 

■ M.-2 HOPLfTE’: Despite its smal sms. Use ГГ8*’ ‘..чва for a variety of duties, nckjdng

DO®» CBtmfe

 

■ Mi-35 ‘HIND-F: Used as a battlefield attack helicopter, the ‘Hind’ has boon constantly —I has seen constdorabk) combat.

 

Ml-34 ‘Hermit’Ml-34 ‘Hermit’Ml-34 ‘Hermit’Ml-34 ‘Hermit’Ml-34 ‘Hermit’

NH Industries

Mi-28 ‘Havoc’

• Anti-tank helicopter • Ail-weather night attack version

Flown for the first time in November 1982, the Mi-28 marked a change in the Soviet approach to battlefield helicopters. The earlier Mi-24 ‘Hind’ was designed to be used liko a dive-bomber rather than for attacking from concealed positions as Western helicopter gunships did. But the ‘Havoc’ is designed to be much belter than the Mi-24 in low-speod and hovering flight, and gives its crews tho option of either type of attack.

▼ Anti-tank missions

For destroying enemy armour the Mi-28 can carry up to 16 Shturm (AT-6 ‘Spiral’) anti-tank missiles and forty 80-mm rockets.

 

Mi-28 ‘Havoc’Mi-28 ‘Havoc’

Mi-28 ‘Havoc’Подпись: ▲ ‘Havoc’ for the 21st century If funding permits, the Russian army would purchase the Mi-28N and the rival Ka-50/-52 combat helicopter. Mi-28 ‘Havoc’▲ Turret-mounted gun

The Mi-28’s 30-mm NPPU-28 cannon has air-to-air capability and can fire up to 900 rounds per minute. Its ammunition is compatible with Russian armoured vehicle weapons.

Mi-28 ‘Havoc’

▲ Production version

Mil upgraded tho oqwpment fit of the Mi-28 to produce the much more capable Mi-28N. This has improved avionics and weaponry and an an-weather capability.

Combat rescue ^

The ‘Havoc’ has a compartment in tho roar fusolago tor tho rescue of combat personnel or for spocial forces insertion. For self-protection, composite armour and a combined chaff/flare and electronic warfare suito are fitted.

FACTS AND FIGURES

► The Mi-28 ‘Havoc-A’ prototypo first flew on 10 November 1982 and appeared at the Parts air show in 1989.

► In emergencies an inflatable crew chute is deployed beneath the door sills.

>■ The fuel tanks of the ‘Havoc’ are
self-sealing and fire retardant.

► Mil plans to develop the MI-28N into the 8- to 10-scat Mi-40 infantry holicopter. which will replace the Mi-24 ‘Hind’.

► Tho Mi-28N can carry the Igla (SA-16 ‘Gimlet’) AAM and new-generation ASMS.

► Tho MI-28N rotorhead contains a 360" millimetre-wave radar system.

Mi-28 ‘Havoc’

Mi-28 ‘Havoc-A’

Туре: heiiccotor gunsh’ro

Powerplanl: two IWO-kW й-200-hn) Klimov TV3-117BMA turboshatts

Maximum speed: 300 km/h (1S6 m p h.)

Range: 470 km (290 mi); ferny 1100 km iS80 mi.)

Hover ceiling: 3600 m m eco ft.) out of ground effect

Weights: empty 8095 kg (17.809 ID); maximum take-off 10-100 kg (40.689 ID.)

Armament: one 30 mm cannon plus up to 16 9-М 114 (AT-6 ‘Spral1) anti-tank mtssJes. 40 80-mm or 130-mm rockets, bombs and two R-73 (AA-11 ‘Archer’) au-to-ar missiles

Dimensions: rotor сіл meter 17.2 m (56 ft 5 ir..i length 16 85 m (55 ft 3 in.)

hesghl 3.82 m (12 ft. 3 in )

rotor d«sc area 232.35 m <2.316 sq ft.)

 

Above: The Klimov TV3- J17 turboshafts power a five-bladed composite main rotor and a scissor-typo tail rotor. This system, and a fenestron tail rotor, wore both first tested on an Mi-24 ‘Hind’ development aircraft.

 

Above: For longer range missions the MI-28 can carry up to four external fuel tanks. Designed to be capable of autonomous battlefield operations, it also has an internal weapons hoist.

 

the nose, and lias a laser rangefinder designator, a missile guidance radar and a more modem range oF ordnance.

 

COMBAT DATA

 

Pctau* fix ttie Havoc’ а provxJod by two f&SO-kW 2200 np) Klrncv tuitxwNittr. with dcwnwwd dolleclwl and shrouded oMvJuut ndjertes. The er orakes ha.-o dust and Vrirqn obtect do fleet с/г. filtnd.

 

Uict Mi-28 u’afntynes і uxi a naaaof-rype. tow – lAntod iai rotor rathet than true conventional type

 

Mi-28 ‘Havoc’
Mi-28 ‘Havoc’

The M 28 саігіпв irAa-red suppressc/s and raai – warning ono loser-wonung rocrxvwt as standard. BtAjoa wngtip pen-.- carry chad and fan isspenser – Th« Mi-28N wtl іпіпхкі’Уі a nWifixitr^wave radar, a FUR txr я tow-ng" клчН TV,-ra a rixVt> wndow 0*n tmrig,

 

Mi-28 ‘Havoc’

ЩШ

/у ■

Щ – – —’

^ 1 <4k

 

The Mi-28 unoe/caniage comprises 3»rgte-wheeiea 720-mni x 320 mm (28 x t2 n) mao urns and a casJarog tah-itieei Afl are motr.’,«kl on shocx-absortjng assemtxius

 

MI-24 МШО О’ 310»Wti(192m. p.h.)

 

M-28 prototvpes nave Been finnn о the West only with B-8 20-round 80 mm rccxnt podo and Sfilurm (AT-6 ‘Sp*a!’l msstes. The Mi-28 .v« prooMVy carry іюм-J ViW-.t (AT – 12i ASMs orxi Igb <SA-161ЛАМЗ.

 

mm NPPU-2? rantven tror. vfues cn ootn lul ana vertical ii»w, A now speoa^sed i" urxJCf ‘.krmioprriwit fcr the W-28N

 

W ctcpen. il tor the M.-40 uUty •wtcootcr vvo use the tuftxxvn iinri rotor systems о» the Mi-28

 

X»-M «rtWWQtf – HOKUM’ «0к*ь (217я. р.х.|

 

MI-28 HftVOC * 200 km 1129 nl, I

 

COMBAT RADIUS

 

Havoc’ over the battlefield

Tie Mi-28 gives Russian force* air-to-air.

E! і tank, attack and combat soarch and

 

AIR DEFENCE: Us. ng its ixidernoae gun o< lightweight air-to-air missiles, the ‘Havoc’ can protect rescue aircraft horn enemy gunships

 

in n nvost versatilo

 

Mi-28 ‘Havoc’

RESCUE: In an i-merijency two peopto can bo carried in a compannterit wtuch is accesscti by a door in tho port side of tho fusetaga. The сотрпддьм.-, s*d to c-j-viyvA5nfortHM<V

 

Mi-28 ‘Havoc’

Mil

Mi-17 ‘Hip’

• Civilian and military use • Many variants • Flown worldwide

Подпись: A Few aircraft aro as versatile or as nigged as the Mi-17. New and improved variants аго being continuously devolopod for all types of civilian, military and humanitarian missions.Mi-17 ‘Hip’Russia’s powerful and versatile

Mil Mi-17, which was based on the phenomonally successful Mi-8, is a truly great design. The ‘Hip-H’ has much greater power than the earlier machine, producing huge improvements in both hovering performance and single-engine flight. The increased capabilities of the Mi-17 make it even more versatile than the Mi-8 and new versions continue to be produced.

SAR Hip-H’ ►

Подпись:Подпись:Mi-17 ‘Hip’Many ‘Hip-H’s are used m tho search-and-rcscuc role, with a powerful winch fitted above the cabin door on the left-hand stdo of Чю fuselage. This Czech aircraft does not carry the optional emergency floatation equipment.

▼ Cabin heating

External fuel tanks arc earned on either side of the fuselage. The tank on tho right, visible on this Czech machine, is longer since the forward section is occupied by a cabin heater.

 

МІ-17М0 weapons ►

A range of anti-tank and air-to-air missiles may be carried on tho strongly braced pylons of tho Kazan-developed Mi-17-MD.

 

Mi-17 ‘Hip’

FACTS AND

► Revealed to the world at tho 1981 Paris air show, the Mi-17 is known by the Russian military as the

► A now rotor hub of titanium alloy was developed for the Ml-17.

► Export customers and Russian civilian operators uso tho Mi-17 designation.

FIGURES

► Individual factories continue to develop now Mi-17 variants, like the Mi-171 produced by the Ulan Ude factory.

► The МІ-17-1ВА variant serves as a flying operating theatre.

► Some Mi-17s may carry a nose-mounted 20-mm cannon.

Mi-17 ‘Hip’

Lett: Kazan Helicopters build the standard Mi – 17M. This one contains a weather radar in tho nose.

 

Type: twtn-turboshah multi-purpose helicopter

Powerplant: two 1434-kW (1.923-hp.) Klimov TV3-117MT lurboshafts

Maximum speed: ?50 km/h <155 m. p.h.)

Range: 495 km (307 mi,) With maximum fuel

Hover ceiling: 1760 m (5.770 ft.) out of ground effect

Weights: empty equipped 7100 kg (15.620 lb.); maximum take-off weight 13000 kg (28.600 lb )

Armament: up to six rocket pods, four ДТ-3 •Sagger’ mastfes and a 12.7-mm (.50 cal I machine-gun

Dimensions:

m*n rotor diameter 21.29 m (69 П. 10 in.) length 25.35 m (83 It. 2 m)

height 4.76 m (15 ft. 7 in.)

main rotor disc area 356.00 m (3.831 sq. ft,)

 

Czechoslovakian military aircraft were divided
between the Czech Republic and Slovakia when
these countries became independent nations. Most
Czech Mi-17s aro painted In this groon/groy scheme

 

In «4! warn ol 0 single crxjme (aduro. tho rwnamng engne automaficaly increases its power Output hem 1434 KW to 1637 kW (1.923 np. to 2.195 hp.|. This. Slows sale tight to continue Filers are nstated tfwad of the engnes lo prevent tne тдв5Тюп of rtawe, although they am rarely seen on Mt-84

 

One of the man recognition pools datmguKtvig tho V – 17 from iho Mi 8 tho reoosrtooed tail rotor. The has been mowd from tho right sido оI the trilboom to Iho loti

 

Vtoncus ivuepona end eoirpment Ms am wxv і on Mi 1 /4. The cne eumbnes <i Ivgh-capacity гвяхо winch with a fusetogo – mcunt—i weapons pylons

 

АЛ M-17s nolixnly adopt a mi-down attitude on tho ground This fuod toi tx/nper prevents damage to the tiki rotor n the cr.-ent ol a heavy landing

 

During very stow speed tight. тресту sideways or backward*, normal means ot measuring airspeed and wt*ude become unrekvbV», To eotvu ttw proWorn u Dopot» radur. whch provides precise right oita d confftned wson the box

 

Troops, cargo and even smefl vehetes are easty loaded wa the two ейтзпе* doors at те rear ot tho fuselage. Hook on ramps allow vehicles to ото straight mio Над coon

 

MAXIMUM SPEE0

 

Mi- 7 development

Ш Mi-tTIfc This lAnn Udo-РіхИ ’Hp-H" is bavcaliy a standard >*• ’ 7M і appoars to liavo boon fitted with a radar and some *>pe Of targeting System under the nose.________________________________________

 

Ш Mi-17Z-2: The Slovak air force operates two ot these AWACS-configured МИ 7s. They are thought to have a secondary Comint and jamming ability

 

■ DAEWOO HEAVY INDUSTRIES МК-Э0: Using the upgraded MI-17M/17Z from the Kazan plant as a basis. Daewoo planned to build the advanced MK-30. Little has been heard of the project.

 

Mi-17 ‘Hip’

Mil

The world’s biggest rotor craft

 

Mi-26 ‘Halo’

 

Type: very targe heavyfifi helicopter

 

Powerplant: two 0-136 turboahaft engines each rated at 8.280-kW (t 1 t03-hp.) and driving an eight-btoded rotor

 

It represent» one ul the greatest advances in rtsary – wing aviation The Mil !i-26 ‘Halo*, fine flown hi 19"!—. l*KtM* unbelievable Stfctigth and lifting power The Mil engineering team, expert* at Wg lielicopter design took Ruvua Ivy storm when ihcir Mil Mi-26 Ix’gan airline and military duties. Then tile ‘Halo went to work, exploiting forestry minerals and hydro – elect ru pwver III the frozen expanse "f Siberia. The Mi-26 is so lutge that it surprised no one when it picked up and moved a four Ічхігооіп house

Піе Mi-26 is hig. I Hit it is also a beauty. Two incredibly

 

chores with the Mi-26. One amazing leal of the Halo was to fly over the burning Chernobyl reactor, dropping chemicals and concrete to try and staunch the radioactive flow.

 

Maximum speed: 295 knvti (183 m p h ) ai 6096 m (20.000 ft.)

 

power! til engines drive its eight-hl. tdc-d main rotor Pilots love this friendly giant: it has a spacious llight deck at floor level with large windows bulged to permit a look at underslung loads, and TV cameras augment die pilots’ all-round view With tile Іч-леІіІ of tins amazing visibility, the crew have little difficulty in carrying out major

 

Above: Tho Mil design bureau has long specialised in hcavylift helicopters. One ot the first to be soon in the West was the Mi-10 ‘Harke’ flying crane.

 

Range: 800 km (497 mi.) at economical cruising speed. 2000 km (1,243 mi.) with au**ary fuel tank

 

Normal ceiling: 4600 m <16.000 ft)

 

Weights: empty 28200 kg (62.170 tb.) «adod 56000 kg (12.346 to.)

  The world’s biggest rotor craft

32 m (105 ft.) 33.73 m (110 ft 8 in.) 8 14 m (26 ft. 8 in) 804.25 m – (8.657 sq. ft l

 

Although the mam rotor ot tho ‘Halo’ is smaller than that of the preceding ‘Hook’, its advanced design generates more lift.

 

This htavyMt helicopter is in service with the Russian air force. Aeroflot, the Ukraine, and the Indian air force.

 

The VC’ Mi-26 has been designed vain the same tttemal rauss – Bocoon as the Syushm «-78 togstc freighter At 3.2 metre© squem (34 eq. ft.), it can hold contane»s or medn/n-saed vehicles w«xxjt ап/ difficulty

 

The eght-ttoded rotor <s ot very до.-апсоо Ое&дп ano of tghtweght but strong construct cr. ft enables the M – 26 to cany trace the toad of its predecessor»

 

Two ЫЯС-kW (11 203-ho) Lotamv turboahaft engnes power the V ‘.’fl ’Ivee oeir. er over 50 per cent more power than tne tfvw erv^nm of the Amenenn &коіаку CH-53E Scpm

 

CWTBnty utibsng ah/Twmzn-Mhwm altoy n its rotors, the •Halo – wf be fitted witncomposte bades in the future

 

СССР-06141

 

COMBAT DATA

 

The > taio’ я eaupceo wf.1 the necessary •Vwe»*tx lo By uv day O’ by ngM. ncurtng * cefT{xrtiif<sed *gnt navigation ■Wem, aromatic ■BN onlrri and a vmwmit radar m Н» ПОМООПв

  The world’s biggest rotor craft

Hato’ can be quckty jurtd tor passenger port, freight, disaster reef ambulance Лйюз Ассеаз to tho cobm is through a large Олт ot clamshell doors at the nvtr. w(h a tower poor acting as о vehcie ramp.

 

Mil’s monsters

f Ш mil mi-6 ’HOOK": F<rst flown in 1957. H>e massive l№6 1 two decades If» world’s largest operational helicopter ■(yarn-, iup wings to provide ext/a lilt m forward flight. It could Carri 5S passengers or up to 12 tons of cargo internally.

 

CH-S3I SurtR SIAUIM

The world’s biggest rotor craft

 

■ MIL Ml-10 HARKE’: Although the cabin of the Mi-6 was txg. И still could not handle outsize toads The Mi-10. which first flew л 1960. was a flying crane variant capable of hoisting loads the size of a bus and up to 14 tons In weight.

 

■ MIL V-12 ’HOMER’: The experimental aircraft «the largest rotary-winged machine ever flown. Powered by two sets of Mi-10 engines and rotors, rt carried a load of 40 tons to 2000 m (6,500 ft.), but control ргсФетз meant that It never entered production.

 

The world’s biggest rotor craftThe world’s biggest rotor craftThe world’s biggest rotor craftThe world’s biggest rotor craft

Mil