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 helicopter<br>Surveillance<br>Anti-submarine helicopter<br>Heliborne early warning
+
|<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; font-weight:bold;"|Unit cost
+
|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; font-weight:bold;"| Crew
+
|style="vertical-align:top; text-align:right;"|'''Crew'''<br>-10C:<br>Others:
|3-4
+
|<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; font-weight:bold;"| Empty weight
+
|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; font-weight:bold;"| Payload
+
|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-10Q drone control helicopter - $42 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 &times; 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 &times; [[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: 4260 litres (3408 kg); five tanks: 5120 litres (4096 kg)<br>
+
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 &times; 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 &times; 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==
Sensors: 360-degree search radar, weather radar, forward optronic search and target turret (FOST; IR, LLTV-CCD, laser), towed magnetic anomaly detector (MAD), sonobuoys (40), dipping medium-low frequency sonar<br>
+
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: 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: 1400 kg of weapons on two stub wings; may be fitted with one door GPMG mount<br>
+
'''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: 360-degree search radar, weather radar, forward optronic search and target turret (FOST; IR, LLTV-CCD, laser)<br>
+
'''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: 1400 kg of weapons on two stub wings; may be fitted with one door GPMG mount<br>
+
'''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

UKIN banner.gif
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.

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


Isselmere-Nieland Defence Industries
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Aircraft:
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Other Equipment:
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