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Manufacturing Capability |
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ADOUR MK 811
Jaguar Aircraft is powered by two Adour MK 804 / MK 811
Engines. MK 811 Engines are manufactured from 1981 under
licence from RR/TM [ Rolls Royce Turbomeca ].
Adour MK 804 Engines are also overhauled and repaired
under the above licence.
Adour Engine is a bypass Jet Engine of modular
construction. The Adour has two-stage low pressure and five-stage high pressure axial flow Compressors which are driven
by separate, single stage high pressure and low pressure
Turbines connected through co-axial shafts, with low
pressure shaft passing through high pressure shaft.
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| Main Characteristics |
| Intake Diameter (m) |
0.564 |
| Length (m) |
2.90 |
| Weight (kg) |
794 |
| Thrust |
2500 (dry)
3737 (wet) |
Specific Fuel Consumption
(kg / kg-hr)
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0.80 |
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GARRETT
331 - 5
The Garrett TPE 331-5 Turbo prop Engine is being
manufactured, overhauled and repaired for various Customers
under licence from Garrett Engine Division of Honey Well
Company [earlier Allied Signal Aerospace Company, USA] since
1988 and belongs to one of the most popular series of small
Turbo prop Engines powering a large number of Commuter and
Corporate Aircraft such as Dornier DO-228.
It has a single shaft
Centrifugal Compressor Engine rated at 715 shaft horse power
at 1591 RPM output speed. Being a reverse flow Gas Turbine
with a small frontal area, it has better dry specifics and
easier airframe integration. Apart from its simplicity of
design and superior performance, the engine features a
propeller control system, anti-icing and foreign object
damage resistance, reverse thrust and negative torque
sensing facilities. The division is also an authorised
service centre for Garrett TPE 331-5 series engines up to -
12.
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| Main Characteristics |
| Maximum Diameter (m) |
0.7 |
| Length (m) |
1.11 |
| Weight (kg) |
164 |
| Power |
715 |
Specific Fuel Consumption
(kg / shp-hr)
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0.268 |
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Artouste
III B
 Artouste
III B Engine powers both Cheetah and Chetak Helicopters.
Manufacture of the Engine commenced in 1962 under licence
from Turbomeca, France.
The Engine has side air
intake, one axial and one centrifugal compressor connected
to a three-stage Turbine. The power output is 550 SHP at
33500 RPM. The reduction Gearbox in the front transfers the
power to Helicopter. More than 665 Engines have been
manufactured and 2950 Engines overhauled and repaired for
various Customers.
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| Main Characteristics |
| Maximum Diameter (m) |
0.50 |
| Length (m) |
1.815 |
| Weight (kg) |
182 |
| Power |
550 |
Specific Fuel Consumption
(kg / shp-hr)
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0.346 |
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| Potential
For Overhaul and Repair |
DART 533 - 2 AND 536 - 2T
 The
Dart series of Engines were manufactured since 1966 under
licence from Rolls Royce, UK. At present, these Engines are
being repaired and overhauled. Two Dart Engines power HS-748
aircraft.
This engine has two-stage Centrifugal Compressors, three-
stage Turbine and utilises water methanol injection to
increase the shaft Horse Power.
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| Main Characteristics |
| Maximum Diameter (m) |
0.960 |
| Length (m) |
2.490 |
| Weight (kg) |
628.6 |
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Power (shp)
533-2
536-2T
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1835 (dry)
1990 (wet)
1835
2040 (wet) |
Specific Fuel Consumption
(kg / shp-hr)
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0.348 |
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ORPHEUS 70105
Orpheus 70105, indigenously modified by HAL, is a
derivative of Orpheus 701 at lower rating and is the Power
Plant for Kiran MK II Aircraft indigenously designed by HAL.
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| Main Characteristics |
| Maximum Diameter (m) |
0.822 |
| Length (m) |
2.290 |
| Weight (kg) |
420 |
| Thrust (kg) |
1875 |
Specific Fuel Consumption
(kg / shp-hr)
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0.348 |
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AVON
Avon is a Turbo Jet Engine designed and developed by Rolls
Royce and is being overhauled / repaired under licence at
HAL from 1959. Avon MK 1 is used in Canberra Trainer
Aircraft. Avon MK 109 is used in Canberra Bomber and Avon MK
203 / 207 power the Hunter Fighter.
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| Main Characteristics |
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Avon
MK 1
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Avon
MK 109
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Avon
MK 203/207
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| Maximum Diameter (m) |
1.07 |
1.09 |
1.05 |
| Length (m) |
2.58 |
3.53 |
3.12 |
| Weight (kg) |
1006 |
1180 |
1310 |
| Thrust (kg) |
2955 |
3363 |
4613 |
Specific Fuel Consumption
(kg / kg-hr)
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0.94 |
0.95 |
0.88 |
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ADOUR MK 804 E
The Adour MK 804 Engine is being repaired and overhauled
under licence from Rolls Royce, UK. This is similar in
construction to the MK 811 engine.
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| Main Characteristics |
| Maximum Diameter (m) |
1.278 |
| Length (m) |
2.990 |
| Weight (kg) |
733 |
| Thrust (kg) |
2343 (dry)
3347 (wet) |
Specific Fuel Consumption
(kg / kg-hr)
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0.79 |
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Gnome 1400 - IT
 The
Gnome 1400 - IT engines being repaired and overhauled under
licence from Rolls Royce, UK and is the Power Plant for
Seaking Helicopter.
It is a Turbo shaft single spool with 10-stage Axial
Compressor, two-stage Turbine and free Power Turbine.
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| Main Characteristics |
| Maximum Diameter (m) |
0.574 |
| Length (m) |
1.376 |
| Weight (kg) |
168 |
| Power (shp) |
1535 |
Specific Fuel Consumption
(kg / shp-hr)
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0.276 |
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