Difference between revisions of "DAS-10 Cormorant"
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! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |Design details | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |Design details | ||
|- | |- | ||
− | |style="vertical-align:top; text-align:right;"|'''Type'''<br>-10C:<br>-10E:<br>-10M:<br>-10W: | + | |style="vertical-align:top; text-align:right;"|'''Type'''<br>-10C:<br>-10D:<br>-10E:<br>-10M:<br>-10W: |
− | |<br>Medium-lift | + | |<br>Medium-lift transport<br>[[Wikipedia:Unmanned aerial vehicle|UAV]]/UGV control<br>Surveillance<br>Maritime patrol<br>Heliborne early warning |
|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[:Category:Corporations|Manufacturer]] | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[:Category:Corporations|Manufacturer]] | ||
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|DAS-10 | |DAS-10 | ||
|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
− | |style="vertical-align:top; text-align:right | + | |style="vertical-align:top; text-align:right;"|'''[[Universal Standard Dollar|Unit cost]]'''<br>-10C:<br>-10D:<br>-10E:<br>-10M:<br>-10W: |
− | |$ million | + | |<br>$30 million<br>$42 million<br>$50 million<br>$44 million<br>$48 million |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates | |style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates | ||
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! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |General characteristics | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |General characteristics | ||
|- | |- | ||
− | |style="vertical-align:top; text-align:right | + | |style="vertical-align:top; text-align:right;"|'''Crew'''<br>-10C:<br>Others: |
− | |3 | + | |<br>3<br>4 |
|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
|style="vertical-align:top; text-align:right;"|'''Length'''<br>Fuselage: | |style="vertical-align:top; text-align:right;"|'''Length'''<br>Fuselage: | ||
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|4.66 m | |4.66 m | ||
|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
− | |style="vertical-align:top; text-align:right | + | |style="vertical-align:top; text-align:right;"|'''Empty weight'''<br>-10C:<br>-10D:<br>-10E:<br>-10M:<br>-10W: |
− | |7873 kg | + | |<br>7873 kg<br>9381.87 kg<br>9369.4 kg<br>10544.36 kg<br>9329 kg |
|- | |- | ||
− | |style="vertical-align:top; text-align:right | + | |style="vertical-align:top; text-align:right;"|'''Payload'''<br>-10C:<br>-10M: |
− | |kg | + | |<br>5443 kg (external)<br>1300 kg |
|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
− | |style="vertical-align:top; text-align:right; font-weight:bold;"| [[Wikipedia:Maximum_Take-Off_Weight|MTOW]] | + | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Maximum_Take-Off_Weight|MTOW]] |
− | |kg | + | |14800 kg |
|- | |- | ||
! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |Flight characteristics | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |Flight characteristics | ||
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|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Speed | |style="vertical-align:top; text-align:right; font-weight:bold;"|Speed | ||
− | |km/h | + | |308 km/h |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability | |style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability | ||
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|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Thrust loadings | |style="vertical-align:top; text-align:right; font-weight:bold;"|Thrust loadings | ||
− | | | + | |54.24 kg/m<small><sup>2</sup></small> |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Fuel fraction | |style="vertical-align:top; text-align:right; font-weight:bold;"|Fuel fraction | ||
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|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Range | |style="vertical-align:top; text-align:right; font-weight:bold;"|Range | ||
− | |km | + | |ca. 1000 km |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling | |style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling | ||
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| | | | ||
|- | |- | ||
− | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" |Armament | + | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;"|Armament |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Internal | |style="vertical-align:top; text-align:right; font-weight:bold;"|Internal | ||
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|''See'' [[#Characteristics|Characteristics]] | |''See'' [[#Characteristics|Characteristics]] | ||
|- | |- | ||
− | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;" | Operators | + | ! colspan=2 style="text-align:center; font-weight:bold; background:#9bc4e2;"|Operators |
|- | |- | ||
|colspan=2 style="vertical-align:top; text-align:center;"|[[Isselmere-Nieland|UKIN]] | |colspan=2 style="vertical-align:top; text-align:center;"|[[Isselmere-Nieland|UKIN]] | ||
|} | |} | ||
− | The '''DAS-10 Cormorant''' [[Wikipedia:Helicopter|helicopter]] series was designed by [[Detmerian Aerospace Dynamics|Detmerian Aerospace]] to replace [[AgustaWestland EH101]] helicopters serving in the [[Isselmere-Nielander Army]] and [[Royal Isselmere-Nieland Navy]] as medium-lift and anti-submarine helicopters as well as for heliborne early warning. Anti-submarine versions of the Cormorant were to have a payload of at least 1500 [[Wikipedia:Kilogram|kg]] — in order to carry at least four weapons of 350 kg on its fuselage-mounted weapon stubs — and have superior sensor systems enabling it to counter enemy submarines and other threats. | + | The '''DAS-10 Cormorant''' [[Wikipedia:Helicopter|helicopter]] series was designed by [[Detmerian Aerospace Dynamics|Detmerian Aerospace]] to replace [[Wikipedia:AgustaWestland EH101|AgustaWestland EH101]] helicopters serving in the [[Isselmere-Nielander Army]] and [[Royal Isselmere-Nieland Navy]] as medium-lift and anti-submarine helicopters as well as for heliborne early warning. Anti-submarine versions of the Cormorant were to have a payload of at least 1500 [[Wikipedia:Kilogram|kg]] — in order to carry at least four weapons of 350 kg on its fuselage-mounted weapon stubs — and have superior sensor systems enabling it to counter enemy submarines and other threats. |
==Characteristics== | ==Characteristics== | ||
'''Variants'''<br> | '''Variants'''<br> | ||
DAS-10C medium lift helicopter - $30 million<br> | DAS-10C medium lift helicopter - $30 million<br> | ||
+ | DAS-10D drone control helicopter - $42 million<br> | ||
DAS-10E signals intelligence helicopter - $50 million<br> | DAS-10E signals intelligence helicopter - $50 million<br> | ||
DAS-10M maritime/anti-submarine helicopter - $44 million<br> | DAS-10M maritime/anti-submarine helicopter - $44 million<br> | ||
− | |||
DAS-10W heliborne early warning (HEW) - $48 million<br> | DAS-10W heliborne early warning (HEW) - $48 million<br> | ||
'''Dimensions:'''<br> | '''Dimensions:'''<br> | ||
Rotor diameter: main: 18.64 m<br> | Rotor diameter: main: 18.64 m<br> | ||
+ | Rotor area: 272.89 m<small><sup>2</sup></small><br> | ||
Fuselage: length (overall): 22.92 m; length (fuselage only): 19.56 m; width: 4.61 m; height: 4.66 m<br> | Fuselage: length (overall): 22.92 m; length (fuselage only): 19.56 m; width: 4.61 m; height: 4.66 m<br> | ||
'''Powerplant'''<br> | '''Powerplant'''<br> | ||
− | Type: 3 × Isselmere Motor Works (IMW) ATG-19S free turbine turboshafts operating through an elastometric hub; main gearbox rating: 5384 kW (7120.07 shp) maximum<br> | + | Type: 3 × [[Isselmere Motor Works]] ('''IMW''') ATG-19S free turbine turboshafts operating through an elastometric hub; main gearbox rating: 5384 kW (7120.07 shp) maximum<br> |
− | Ratings (per engine): take-off: 1764 kW (2365.57 shp); 60 min. intermediate rated power (IRP): 1670 kW (2239.58 shp); 2.5 min. contingency one-engine inoperable (OEI): 1864.25 kW (2500 shp); continuous: 1554 kW (2084 shp)<br> | + | Ratings (per engine): take-off: 1764 [[Wikipedia:Kilowatt|kW]] (2365.57 [[Wikipedia:Horsepower|shp]]); 60 min. intermediate rated power ('''IRP'''): 1670 kW (2239.58 shp); 2.5 min. contingency one-engine inoperable ('''OEI'''): 1864.25 kW (2500 shp); continuous: 1554 kW (2084 shp)<br> |
'''Capacity'''<br> | '''Capacity'''<br> | ||
− | Fuel: three tanks: 3230 litres (2584 kg); four tanks: | + | Fuel: three tanks: 3230 litres (2584 kg); four tanks: 4100 litres (3280 kg); five tanks: 5124 litres (4099.2 kg)<br> |
Cabin: 29 m<small><sup>3</sup></small><br> | Cabin: 29 m<small><sup>3</sup></small><br> | ||
External cargo sling points: 3000 kg, 4536 kg, 5443 kg<br> | External cargo sling points: 3000 kg, 4536 kg, 5443 kg<br> | ||
==DAS-10C medium lift helicopter== | ==DAS-10C medium lift helicopter== | ||
− | The '''DAS-10C''' ''medium-lift helicopter'' ('''MLH''') variant is commonly referred to as the base model of the design. | + | The '''DAS-10C''' ''medium-lift helicopter'' ('''MLH''') variant is commonly referred to as the base model of the design. Despite being able to transport up to a platoon (43 soldiers), both the INA and the RINM prefer it to transport half-platoon detachments as well as any other equipment operational contigencies might require. |
− | Weights: empty: 7873 kg; clean: 11045 kg (4 fuel tanks full); armed (2 × 7.62mm GPMG side guns): 11105.2 kg; troop carrier: 14555 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg<br> | + | '''Service designation:''' HC.3<br> |
− | Payload: 27 troops, 3000 kg (internal), 5443 kg external (slung)<br> | + | '''Weights:''' empty: 7873 kg; clean: 11045 kg (4 fuel tanks full); armed (2 × 7.62mm GPMG side guns): 11105.2 kg; troop carrier: 14555 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg<br> |
+ | '''Payload:''' 27 troops, 3000 kg (internal), 5443 kg external (slung)<br> | ||
==DAS-10D drone control helicopter== | ==DAS-10D drone control helicopter== | ||
+ | The '''DAS-10D''' ''drone control'' ('''DCH''') variant was designed to support the operation of uncrewed aerial and/or ground vehicles, in particular those used by the [[Isselmere-Nielander Army]] and the [[Royal Isselmere-Nieland Marines]]. | ||
+ | |||
+ | '''Service designation:''' HQ.5<br> | ||
==DAS-10E signals intelligence and surveillance helicopter== | ==DAS-10E signals intelligence and surveillance helicopter== | ||
+ | '''Service designation:''' HE.4<br> | ||
==DAS-10M maritime patrol helicopter== | ==DAS-10M maritime patrol helicopter== | ||
− | + | The [[Royal Isselmere-Nieland Navy]] wanted the DAS-10M maritime patrol variant to be able to carry four air-dropped [[GWS.63 Barracuda]] [[Wikipedia:Torpedo|torpedo]]es with four full fuel tanks with 4100 [[Wikipedia:Litre|litre]]s of [[Wikipedia:JP-8|JP-8]]. In practice, most RINN anti-submarine patrols operate with three tanks containing a total of 3230 litres as well as the four lightweight torpedoes, although in wartime greater endurance takes precedence over payload. | |
− | Weights: | + | |
− | Payload: | + | '''Service designation:''' HM.1<br> |
+ | '''Sensors:''' 360° search radar (ARS.282 ''Scrimshaw''), weather radar (ARN.239), forward optronic search and target turret ('''FOST''', ASU.280; [[Wikipedia:Thermal imaging|infra-red]], low light-level television-charge coupled device ('''LLLTV-CCD'''), laser), towed magnetic anomaly detector ('''MAD''', ASQ.117), [[Wikipedia:Sonobuoy|sonobuoy]]s (40), dipping medium-low frequency [[Wikipedia:Sonar|sonar]] (AQS.209)<br> | ||
+ | '''Weights:''' Empty: 9208.68 kg; clean: 12510.68 kg; equipped (sonobuoys): 13218.28 kg; mission weight (4 x GWS.63A Barracuda torpedoes): 14518.28 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg<br> | ||
+ | '''Payload:''' 1300 kg of weapons on two stub wings; may be fitted with one or two door [[Wikipedia:General purpose machine gun|general purpose machine gun]] mount(s)<br> | ||
==DAS-10W heliborne early warning== | ==DAS-10W heliborne early warning== | ||
Heliborne early warning ('''HEW''') | Heliborne early warning ('''HEW''') | ||
− | Sensors: | + | '''Service designation:''' HEW.2<br> |
− | Weights: empty: 9367.4 kg; 12671.4 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg<br> | + | '''Sensors:''' 360° search radar (ARS.283), weather radar (ARN.239), FOST turret (ASU.280; IR, LLTV-CCD, laser)<br> |
− | Payload: | + | '''Weights:''' empty: 9367.4 kg; 12671.4 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg<br> |
+ | '''Payload:''' 1300 kg of weapons on two stub wings; may be fitted with one door GPMG mount<br> | ||
{{Isselmere-Nieland Defence Industries}} | {{Isselmere-Nieland Defence Industries}} | ||
{{Isselmere-Nieland}} | {{Isselmere-Nieland}} | ||
[[Category:Hardware]] | [[Category:Hardware]] |
Latest revision as of 02:12, 21 July 2007
Profile (n/a) | |
DAS-10 Cormorant | |
---|---|
Design details | |
Type -10C: -10D: -10E: -10M: -10W: |
Medium-lift transport UAV/UGV control Surveillance Maritime patrol Heliborne early warning |
Manufacturer | Detmerian Aerospace |
Design No. | DAS-10 |
Unit cost -10C: -10D: -10E: -10M: -10W: |
$30 million $42 million $50 million $44 million $48 million |
Service dates | 2005-present |
General characteristics | |
Crew -10C: Others: |
3 4 |
Length Fuselage: |
22.92 m 19.56 m |
Rotor diameter | 18.64 m |
Width | 4.61 m (w/ stub wings) |
Height | 4.66 m |
Empty weight -10C: -10D: -10E: -10M: -10W: |
7873 kg 9381.87 kg 9369.4 kg 10544.36 kg 9329 kg |
Payload -10C: -10M: |
5443 kg (external) 1300 kg |
MTOW | 14800 kg |
Flight characteristics | |
Engines | 3 × IMW ATG-19S |
Speed | 308 km/h |
Manoeuvrability | g |
Thrust loadings | 54.24 kg/m2 |
Fuel fraction | |
Range | ca. 1000 km |
Ceiling | m |
Rate of climb | |
Armament | |
Internal | See Characteristics |
External | See Characteristics |
Operators | |
UKIN |
The DAS-10 Cormorant helicopter series was designed by Detmerian Aerospace to replace AgustaWestland EH101 helicopters serving in the Isselmere-Nielander Army and Royal Isselmere-Nieland Navy as medium-lift and anti-submarine helicopters as well as for heliborne early warning. Anti-submarine versions of the Cormorant were to have a payload of at least 1500 kg — in order to carry at least four weapons of 350 kg on its fuselage-mounted weapon stubs — and have superior sensor systems enabling it to counter enemy submarines and other threats.
Contents
Characteristics
Variants
DAS-10C medium lift helicopter - $30 million
DAS-10D drone control helicopter - $42 million
DAS-10E signals intelligence helicopter - $50 million
DAS-10M maritime/anti-submarine helicopter - $44 million
DAS-10W heliborne early warning (HEW) - $48 million
Dimensions:
Rotor diameter: main: 18.64 m
Rotor area: 272.89 m2
Fuselage: length (overall): 22.92 m; length (fuselage only): 19.56 m; width: 4.61 m; height: 4.66 m
Powerplant
Type: 3 × Isselmere Motor Works (IMW) ATG-19S free turbine turboshafts operating through an elastometric hub; main gearbox rating: 5384 kW (7120.07 shp) maximum
Ratings (per engine): take-off: 1764 kW (2365.57 shp); 60 min. intermediate rated power (IRP): 1670 kW (2239.58 shp); 2.5 min. contingency one-engine inoperable (OEI): 1864.25 kW (2500 shp); continuous: 1554 kW (2084 shp)
Capacity
Fuel: three tanks: 3230 litres (2584 kg); four tanks: 4100 litres (3280 kg); five tanks: 5124 litres (4099.2 kg)
Cabin: 29 m3
External cargo sling points: 3000 kg, 4536 kg, 5443 kg
DAS-10C medium lift helicopter
The DAS-10C medium-lift helicopter (MLH) variant is commonly referred to as the base model of the design. Despite being able to transport up to a platoon (43 soldiers), both the INA and the RINM prefer it to transport half-platoon detachments as well as any other equipment operational contigencies might require.
Service designation: HC.3
Weights: empty: 7873 kg; clean: 11045 kg (4 fuel tanks full); armed (2 × 7.62mm GPMG side guns): 11105.2 kg; troop carrier: 14555 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg
Payload: 27 troops, 3000 kg (internal), 5443 kg external (slung)
DAS-10D drone control helicopter
The DAS-10D drone control (DCH) variant was designed to support the operation of uncrewed aerial and/or ground vehicles, in particular those used by the Isselmere-Nielander Army and the Royal Isselmere-Nieland Marines.
Service designation: HQ.5
DAS-10E signals intelligence and surveillance helicopter
Service designation: HE.4
DAS-10M maritime patrol helicopter
The Royal Isselmere-Nieland Navy wanted the DAS-10M maritime patrol variant to be able to carry four air-dropped GWS.63 Barracuda torpedoes with four full fuel tanks with 4100 litres of JP-8. In practice, most RINN anti-submarine patrols operate with three tanks containing a total of 3230 litres as well as the four lightweight torpedoes, although in wartime greater endurance takes precedence over payload.
Service designation: HM.1
Sensors: 360° search radar (ARS.282 Scrimshaw), weather radar (ARN.239), forward optronic search and target turret (FOST, ASU.280; infra-red, low light-level television-charge coupled device (LLLTV-CCD), laser), towed magnetic anomaly detector (MAD, ASQ.117), sonobuoys (40), dipping medium-low frequency sonar (AQS.209)
Weights: Empty: 9208.68 kg; clean: 12510.68 kg; equipped (sonobuoys): 13218.28 kg; mission weight (4 x GWS.63A Barracuda torpedoes): 14518.28 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg
Payload: 1300 kg of weapons on two stub wings; may be fitted with one or two door general purpose machine gun mount(s)
DAS-10W heliborne early warning
Heliborne early warning (HEW)
Service designation: HEW.2
Sensors: 360° search radar (ARS.283), weather radar (ARN.239), FOST turret (ASU.280; IR, LLTV-CCD, laser)
Weights: empty: 9367.4 kg; 12671.4 kg; maximum take-off: 14800 kg; alternative gross weight: 15800 kg
Payload: 1300 kg of weapons on two stub wings; may be fitted with one door GPMG mount
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