Aircraft / Utility helicopters / Bell 205
Bell 205
General Facts
- TYPE
Transport helicopter - ORIGIN
United States - NICKNAMES
UH-1 Iroquois (US military version)
HU-1 Huey (early designation/nickname)
CH-118 (UH-1D in Canadian service)
Cheetah (AB-205 in Zimbabwan service)
EM-2 (AB-205 in Italian service)
HE.10B (AB-205 in Spanish service) - DESIGNED
1960 - 1961 - DESIGNER
Bell - PRODUCTION
1963 - early 1980's - PRODUCERS
Germany - Dornier
Italy - Agusta-Bell
Japan - Fuji
Taiwan - AIDC
United States - Bell - QUANTITY
12.000 of all Bell 205 models, including license production and civilian sales - UNIT COST
About $ 345.000 US Army procurement cost for UH-1H in 1965
About $ 800.000 for UH-1H export in 1975
About $ 1.1 million of UH-1H production in Japan in 1975 - CHARACTERISTICS
Limited production costs
Large internal volume
Good carrying capacity
Limited power in early models
Introduction
The Bell 205 is a transport helicopter of US origin. It was developed in the early 1960's by Bell to provide an increased transport capability over the Bell 204. In its US military UH-1 Iroquois designation and Huey nickname it became an icon for the Vietnam war. It is one of the most numerous transport helicopters in the world. The design lives on in the twin engine Bell 212 and Bell 412.
Layout
The Bell 205 is a stretched version of the earlier Bell 204, but is nearly identical in all other aspects. Compared to the Bell 204 the cabin has been lengthened by 1.04 m to increase the internal carrying capacity. This meant that wider doors were needed. The Bell 205 also features longer rotor blades and has a lengthened tail to accomodate them. The single engine setup has been retained. At the 1.100 hp engine as used in the Bell 204 was retained, but a more powerful 1.400 hp engine was installed.
Firepower
Most Bell 205 are fitted with a pintle mounted 7.62mm M60 machine gun on each side or are unarmed. Unlike the Bell 204 no dedicated gunship versions were created from the Bell 205. With the use of special kits it is possible to mount 7 or 19 round 70mm FFAR pods and M134 miniguns, although these configurations are rare outside US service.
Cargo
The main purpose of the Bell 205 is troop transport. When only a single pilot is used it is possible to carry 14 troops. This is a phenomenal number for a single engine Vietnam era helicopter. In the medevac role it is possible to carry six stretchers. The cargo capacity is 1.7 t. This means that when armament mounts are fitted the carry capacity is significantly reduced.
Mobility
The Bell 205 has a maximum speed of 217 km/h and a range of just over 500 km. The models with the uprated 1.400 hp engine have the same maximum flight characteristics but perform better within those limits due to their additional power.
Users
The main user of the Bell 205 was the US military and over 7.000 UH-1 served in Vietnam. Nowadays all single engine UH-1 have been replaced, most by the UH-60 Blackhawk. The UH-1 and Bell 205 models were widely exported and large quantities have been produced under license, most of them by Agusta-Bell in Italy. Today large quantities remain in service all over the world, most of them can be found in South America and Asia.
UH-1 Iroquois
UH-1D: Original military production model of the Model 205 with the same 1.100 hp engine as used in the Bell 204.
UH-1H: Improved military model with 1.400 hp engine. This is the most numerous version of the Bell 205 family.
Type | Transport helicopter |
---|---|
Crew | 15 in total (1 - 4 pilot/crew, 11 - 14 troops) |
Lenght | 17.40 m overall |
Width | ? |
Height | 4.39 m |
Weight | 2.4 t empty, 4.1 t gross weight, 4.3 t MTOW |
Rotors | Two blade main rotor, two blade tail rotor |
Diameter | 14.63 m main rotor, 2.59 m tail rotor |
Disc area | 168 m2 main, 5.3 m2 tail |
Chord | ? |
Powerplant | 1x Lycoming T53-L-11 turboshaft, 1.100 hp |
Speed | 217 km/h max, 201 km/h cruise |
Range | 507 km |
---|---|
Fuel | ? |
Climb rate | 8.9 m/s |
Ceiling | 5.9 km |
Endurance | ? |
Landing gear | Skids |
Armor | None |
Cargo | Up to 14 troops 6 stretchers 1.7 t cargo |
Avionics | Standard flight controls |
Self defense | None |
Remarks | - |
Weapon systems | 2x 7.62mm M60 machine gun 70mm FFAR pods |
Fixed weapons | - |
---|---|
Hardpoints | - |
Option 1 | Optional 7.62mm M60 machine gun in each door |
Option 2 | Optional M21 MAMEE with M134 and 3.000 round and 7x 70mm FFAR on reach side |
Option 3 | Optional 7 or 19 round FFAR pod on special mount on each side |
Option 4 | - |
Option 5 | - |
Option 6 | - |
Option 7 | - |
Option 8 | - |
Type | Transport helicopter |
---|---|
Crew | 15 in total (1 - 4 pilot/crew, 11 - 14 troops) |
Lenght | 17.62 m rotors turning, 12.77 m fuselage |
Width | ? |
Height | 4.39 m |
Weight | 2.4 t empty, 4.1 t gross weight, 4.3 t MTOW |
Rotors | Two blade main rotor, two blade tail rotor |
Diameter | 14.63 m main rotor, 2.59 m tail rotor |
Disc area | 168 m2 main, 5.3 m2 tail |
Chord | ? |
Powerplant | 1x Lycoming T53-L-13 turboshaft, 1.400 hp |
Speed | 217 km/h max, 201 km/h cruise |
Range | 507 km |
---|---|
Fuel | ? |
Climb rate | ? |
Ceiling | ? |
Endurance | ? |
Landing gear | Skids |
Armor | None |
Cargo | Up to 14 troops 6 stretchers |
Avionics | Standard flight controls |
Self defense | None |
Remarks | - |
Weapon systems | 2x 7.62mm machine gun |
Fixed weapons | - |
---|---|
Hardpoints | - |
Option 1 | Optional 7.62mm M60 machine gun in each door |
Option 2 | Optional M21 MAMEE with M134 and 3.000 round and 7x 70mm FFAR on reach side |
Option 3 | Optional 7 or 19 round FFAR pod on special mount on each side |
Option 4 | - |
Option 5 | - |
Option 6 | - |
Option 7 | - |
Option 8 | - |
Bell 205
Bell 205: Civilian model of the UH-1D, also exported for military use.
Bell 205A1: Civilian model of the UH-1H, widely exported for military use.
- Specifications:
- Bell 205A1
Type | Transport helicopter |
---|---|
Crew | 15 in total (1 - 4 pilot/crew, 11 - 14 troops) |
Lenght | 17.62 m rotors turning, 12.77 m fuselage |
Width | ? |
Height | 4.41 m |
Weight | 2.52 t empty, 4.1 normal, 4.31 t MTOW |
Rotors | Two blade main rotor, two blade tail rotor |
Diameter | 14.63 m main rotor, 2.59 m tail rotor |
Disc area | 168 m2 main, 5.3 m2 tail |
Chord | ? |
Powerplant | 1x Textron Lycoming T-53-L-13 turboshaft, 1.400 hp derated to 1.250 hp |
Speed | 204 km/h |
Range | 511 km |
---|---|
Fuel | 844 L |
Climb rate | 8.1 m/s |
Ceiling | 4.1 km |
Endurance | ? |
Landing gear | Skids, 2.91 m track |
Armor | None |
Cargo | Up to 14 troops 6 stretchers |
Avionics | Standard flight controls |
Self defense | None |
Remarks | - |
Weapon systems | 2x 7.62mm machine gun |
Fixed weapons | - |
---|---|
Hardpoints | - |
Option 1 | Optional 7.62mm machine gun in each door |
Option 2 | - |
Option 3 | - |
Option 4 | - |
Option 5 | - |
Option 6 | - |
Option 7 | - |
Option 8 | - |
AB-205
AB-205: Italian production version of the UH-1D.
AB-205A: AB-205 with longer rotor blades and various minor improvements.
AB-205A-1: Italian production model of the UH-1H with longer rotor blades.
- Specifications:
- AB-205A-1
Type | Transport helicopter |
---|---|
Crew | 15 in total (1 - 4 pilot/crew, 11 - 14 troops) |
Lenght | 17.98 m rotors turning, 12.78 m fuselage |
Width | 2.84 m stabiliser span |
Height | 4.48 m overall |
Weight | 2.18 t empty, 3.86 t normal, 4.31 t MTOW |
Rotors | Two blade main rotor, two blade tail rotor |
Diameter | 14.72 m main rotor, 2.59 m tail rotor |
Disc area | 170 m2 main, 5.3 m2 tail |
Chord | ? |
Powerplant | 1x Textron Lycoming T-53-L-13 turboshaft, 1.400 hp derated to 1.250 hp |
Speed | 222 km/h max at sea level, 204 km/h at altitude |
Range | 580 km |
---|---|
Fuel | 833 L |
Climb rate | 9.2 m/s |
Ceiling | 4.6 km |
Endurance | 3 hour 48 minutes |
Landing gear | Skids, 2.60 m track |
Armor | None |
Cargo | Up to 14 troops 6 stretchers 1.4 t cargo |
Avionics | Standard flight controls |
Self defense | None |
Remarks | - |
Weapon systems | 2x 7.62mm machine gun |
Fixed weapons | - |
---|---|
Hardpoints | - |
Option 1 | Optional 7.62mm machine gun in each door |
Option 2 | - |
Option 3 | - |
Option 4 | - |
Option 5 | - |
Option 6 | - |
Option 7 | - |
Option 8 | - |