Difference between revisions of "GWS.52 Pelican"

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{| border=0 cellspacing=0 cellpadding=4 style="float:right; margin:0 0 .5em 1em; width:250px; background:#fff; border-collapse:collapse; border:1px solid #999; font-size:85%; line-height:1.5; "
 
{| border=0 cellspacing=0 cellpadding=4 style="float:right; margin:0 0 .5em 1em; width:250px; background:#fff; border-collapse:collapse; border:1px solid #999; font-size:85%; line-height:1.5; "
 
|- style="background:#f0f0f0; text-align:center; width=250px;"
 
|- style="background:#f0f0f0; text-align:center; width=250px;"
| align=center colspan=2 |http://www.nationstates.net/images/flags/kiribati--53.jpg
+
| align=center colspan=2 |[[Image:UKIN_banner.gif]]
 
|-style="background:#f0f0f0;"
 
|-style="background:#f0f0f0;"
 
| align=center colspan=2 | '''Profile (n/a)'''
 
| align=center colspan=2 | '''Profile (n/a)'''
Line 20: Line 20:
 
|LMR-28
 
|LMR-28
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Defence Procurement Agency (Isselmere-Nieland)#41-60|DPA No.]]
+
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Defence Procurement Agency (Isselmere-Nieland)#41-60|GSI No.]]
 
|GWS.52
 
|GWS.52
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Currency|Unit cost]]
+
|style="vertical-align:top; text-align:right;"|'''[[Currency|Unit cost]]'''<br>[[Wikipedia:Air-to-surface_missile|ASM]]:<br>[[Wikipedia:Surface-to-surface_missile|SSM]], [[Wikipedia:SLCM|SLCM]]:
|$1.38 million ([[Wikipedia:Air-to-surface_missile|ASM]])<br>$1.4 million (LC)
+
|<br>$1.38 million<br>$1.4 million
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates
Line 31: Line 31:
 
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |General characteristics
 
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |General characteristics
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"| Length  
+
|style="vertical-align:top; text-align:right;"|'''Length'''<br>ASM:<br>SSM, SLCM:<br>LC:
| 8 m (ASM)<br>8.52 m ([[Wikipedia:Surface-to-surface_missile|SSM]])<br>8.9 m (LC)
+
|<br>8 m<br>8.52 m<br>8.9 m
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"| Diameter
+
|style="vertical-align:top; text-align:right;"|'''Diameter'''<br>Missile:<br>LC:
| 60 cm (core)<br>65 cm (LC)
+
|<br>65 cm<br>70 cm
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"| Finspan
+
|style="vertical-align:top; text-align:right; font-weight:bold;"|Finspan
| 75 cm
+
|75 cm
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"| Wingspan
+
|style="vertical-align:top; text-align:right; font-weight:bold;"|Wingspan
| 196 cm
+
|196 cm
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"| Launch mass
+
|style="vertical-align:top; text-align:right;"|'''Launch mass'''<br>AGM:<br>SSM, SLCM:
| 2500 kg (AGM)<br>3000 kg (other)
+
|<br>2500 kg<br>3000 kg
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|Launch canister
+
|style="vertical-align:top; text-align:right;"|'''Launch canister'''<br>GWLS.39M, sub:<br>GWLS.35M2/3:
| 3800 kg
+
|<br>3800 kg<br>3942.53 kg
 
|-
 
|-
 
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Flight characteristics
 
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Flight characteristics
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion
+
|style="vertical-align:top; text-align:right;"|'''Propulsion'''<br>Stage 1:<br>Stage 2:
|RBS.52 solid rocket booster<br>ATG-15R turbo-ramjet
+
|<br>RBS.52 solid rocket booster<br>ATG-15R turbo-ramjet
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control
Line 63: Line 63:
 
|&gt;12''[[Wikipedia:Acceleration_due_to_gravity|g]]''
 
|&gt;12''[[Wikipedia:Acceleration_due_to_gravity|g]]''
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|Range
+
|style="vertical-align:top; text-align:right;"|'''Range'''<br>AGM:<br>LC:
|570 km (AGM)<br>325 km (LC)
+
|<br>570 km<br>325 km
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling
Line 71: Line 71:
 
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Guidance and payload
 
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Guidance and payload
 
|-
 
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|Guidance
+
|style="vertical-align:top; text-align:right;"|'''Guidance'''<br>Midcourse:<br><br>Terminal:
|'''Midcourse:'''
+
|<br>[[Wikipedia:Global_Positioning_System|GPS]]/[[Wikipedia:Inertial_guidance_system|INS]], [[Autonomous Operation Situational Awareness Module|AOSAM]], command uplink<br>Dual-mode [[Wikipedia:Radar|radar]] with [[Wikipedia:Imaging_infrared|IIR]] and automatic target recognition
*[[Wikipedia:Global_Positioning_System|GPS]]/[[Wikipedia:Inertial_guidance_system|INS]], [[Autonomous Operation Situational Awareness Module|AOSAM]], command uplink
+
'''Terminal:'''
+
*Dual-mode [[Wikipedia:Radar|radar]] with [[Wikipedia:Imaging_infrared|IIR]] and automatic target recognition
+
 
|- style="background:#f0f0f0;"
 
|- style="background:#f0f0f0;"
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Warhead|Warhead]]
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Warhead|Warhead]]
Line 83: Line 80:
 
|Timed penetrator, contact
 
|Timed penetrator, contact
 
|-
 
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Launch platforms
+
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Launch platforms
 
|-
 
|-
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Navy|Ship]]
 
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Navy|Ship]]
Line 91: Line 88:
 
|L13/52
 
|L13/52
 
|-
 
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Operators
+
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |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]]
Line 113: Line 110:
 
Air: AGM.52A<br>
 
Air: AGM.52A<br>
 
Ground: FGM.52A<br>
 
Ground: FGM.52A<br>
Sub-surface: UGM.52<br>
+
Sub-surface: UGM.52A<br>
 
Surface ship: MGM.52A<br>
 
Surface ship: MGM.52A<br>
 
'''Dimensions:'''<br>
 
'''Dimensions:'''<br>
Length: 8m (ASM); 8.52m (SSM); 8.9m (LC)<br>
+
Length: 8 m ([[Wikipedia:Air-to-surface_missile|ASM]]); 8.52 m ([[Wikipedia:Surface-to-surface_missile|SSM]] or [[Wikipedia:SLCM|SLCM]])<br>
Diameter: 60cm (core); 65cm (LC)<br>
+
Diameter: 60 cm (core)<br>
Finspan (deployed): 75cm
+
Finspan (deployed): 75 cm<br>
Wingspan (deployed): 1.96m<br>
+
Wingspan (deployed): 1.96 m<br>
 +
Launch canister (LC):<br>
 +
—L13/52, GWLS.39M, or sub (cylindrical): 65 cm diameter; 890 cm high<br>
 +
—GWLS.35M2/M3 (l &times; w &times; h): 65 cm/70 cm &times; 65 cm/70 cm &times; 900 cm<br>
 
'''Mass:'''<br>
 
'''Mass:'''<br>
Air launched version: 2500kg<br>
+
Air launched version: 2500 kg<br>
 
Surface-/Submerged-launched version: 3000 kg (launch weight)<br>
 
Surface-/Submerged-launched version: 3000 kg (launch weight)<br>
Launch canister (LC): 3800 kg<br>
+
Launch canister:<br>
 +
—L13/52, GWLS.39M, or sub (loaded): 3800 kg<br>
 +
—GWLS.35M2/M3 (loaded): 3942.53 kg<br>
 
'''Warhead:''' 250 kg APHE<br>
 
'''Warhead:''' 250 kg APHE<br>
'''Propulsion:'''
+
'''Propulsion:'''<br>
Booster: RBS.52
+
Booster: RBS.52<br>
 
Missile: ATG-15R turbo-ramjet<br>
 
Missile: ATG-15R turbo-ramjet<br>
 
'''Guidance:'''<br>
 
'''Guidance:'''<br>
Line 140: Line 142:
 
'''Ceiling:''' 15 km; attack altitude 10-5 m and lower (depending on sea states)<br>
 
'''Ceiling:''' 15 km; attack altitude 10-5 m and lower (depending on sea states)<br>
 
'''Speed:''' [[Wikipedia:Mach|Mach]] 1.65 (supercruise); Mach 3.22+ (terminal)<br>
 
'''Speed:''' [[Wikipedia:Mach|Mach]] 1.65 (supercruise); Mach 3.22+ (terminal)<br>
'''Cost:''' $1.225 million<br>
+
'''Cost:''' $1.225 million
  
 
==GWS.52-2==
 
==GWS.52-2==
Line 150: Line 152:
 
Surface: MGM.52B<br>
 
Surface: MGM.52B<br>
 
'''Dimensions:'''<br>
 
'''Dimensions:'''<br>
Length: 8m (ASM), 8.52m (SSM), 8.9m (LC)<br>
+
Length: 8m (ASM), 8.52m (SSM)<br>
Diameter: 60cm (core), 65cm (LC)<br>
+
Diameter: 60cm (core)<br>
Finspan (ASM/deployed): 75cm
+
Finspan (ASM/deployed): 75cm<br>
 
Wingspan (deployed): 1.96m<br>
 
Wingspan (deployed): 1.96m<br>
 +
Launch canister (LC):<br>
 +
—L13/52, GWLS.39M, or sub (cylindrical): 65 cm diameter; 890 cm high<br>
 +
—GWLS.35M2/M3 (l &times; w &times; h): 65 cm/70 cm &times; 65 cm/70 cm &times; 943 cm<br>
 
'''Mass:'''<br>
 
'''Mass:'''<br>
 
Air-launched: 2500kg (2.5t)<br>
 
Air-launched: 2500kg (2.5t)<br>
Surface-/Submerged-launched: (launch weight) 3000 kg (3t), (LC) 3800 kg (3.8t)<br>
+
Surface-/Submerged-launched: 3000 kg<br>
 +
Launch canister:<br>
 +
—L13/52, GWLS.39M, or sub (loaded): 3800 kg<br>
 +
—GWLS.35M2/M3 (loaded): 3942.53 kg<br>
 
'''Warhead:''' 300 kg APHE<br>
 
'''Warhead:''' 300 kg APHE<br>
'''Propulsion:'''
+
'''Propulsion:'''<br>
Boosters: RBS.52-2
+
Boosters: RBS.52B<br>
 
Missile: ATG-15R2 turbo-ramjet<br>
 
Missile: ATG-15R2 turbo-ramjet<br>
 
'''Guidance:'''<br>
 
'''Guidance:'''<br>
Line 173: Line 181:
 
'''Ceiling:''' 15 km; attack altitude 10-5 m and lower (depending on sea states)<br>
 
'''Ceiling:''' 15 km; attack altitude 10-5 m and lower (depending on sea states)<br>
 
'''Speed:''' Mach &gt;2.5 (cruise); Mach &gt;3.22 (terminal)<br>
 
'''Speed:''' Mach &gt;2.5 (cruise); Mach &gt;3.22 (terminal)<br>
'''Cost:''' (ASM): $1.38 million; (LC): $1.4 million<br>
+
'''Cost:''' (ASM): $1.38 million; (LC): $1.4 million
  
 
==GWS.52-3==
 
==GWS.52-3==
Line 183: Line 191:
 
Surface: MGM.52C<br>
 
Surface: MGM.52C<br>
 
'''Dimensions:'''<br>
 
'''Dimensions:'''<br>
Length: ''tbd'', 8.9m (LC)<br>
+
Length: ''tbd''<br>
Diameter: 60cm (core), 65cm (LC)<br>
+
Diameter: 60cm (core)<br>
 
Finspan (ASM/deployed): 75cm<br>
 
Finspan (ASM/deployed): 75cm<br>
 
Wingspan (deployed): 1.96m <br>
 
Wingspan (deployed): 1.96m <br>
 +
Launch canister (LC):<br>
 +
—L13/52, GWLS.39M, or sub (cylindrical): 65 cm diameter; 890 cm high<br>
 +
—GWLS.35M2/M3 (l &times; w &times; h): 65 cm/70 cm &times; 65 cm/70 cm &times; 943 cm<br>
 
'''Mass:'''<br>
 
'''Mass:'''<br>
 
AGM: ''tbd''<br>
 
AGM: ''tbd''<br>
 
FGM, MGM, UGM: ''tbd''<br>
 
FGM, MGM, UGM: ''tbd''<br>
 +
Launch canister:<br>
 +
—GWLS.39M or sub (empty): 800 kg<br>
 +
—GWLS.35M2/M3 (empty): 942.53 kg<br>
 
'''Warhead:''' ''tbd''<br>
 
'''Warhead:''' ''tbd''<br>
'''Propulsion:'''
+
'''Propulsion:'''<br>
Boosters: RBS.52A2 (ASM); RBS.52J2 (other)
+
Boosters: RBS.52C (ASM); RBS.52D (other)<br>
 
Missile: ATG-29J turbojet<br>
 
Missile: ATG-29J turbojet<br>
 
'''Guidance:'''<br>
 
'''Guidance:'''<br>
Line 206: Line 220:
 
'''Ceiling:''' &gt;26 km<br>
 
'''Ceiling:''' &gt;26 km<br>
 
'''Speed:''' [[Wikipedia:Mach|Mach]] 3.77 (max., 11-25 km altitude), Mach 3.22 (terminal, diving), Mach 3.07 (ASL)<br>
 
'''Speed:''' [[Wikipedia:Mach|Mach]] 3.77 (max., 11-25 km altitude), Mach 3.22 (terminal, diving), Mach 3.07 (ASL)<br>
'''Cost:''' ''tbd''<br>
+
'''Cost:''' ''tbd''
  
 
{{Surface-to-surface missiles}}
 
{{Surface-to-surface missiles}}
 
{{Isselmere-Nieland Defence Industries}}
 
{{Isselmere-Nieland Defence Industries}}
 
{{Isselmere-Nieland}}
 
{{Isselmere-Nieland}}

Latest revision as of 15:22, 15 August 2007

UKIN banner.gif
Profile (n/a)
Pelican
Design details (GWS.52-2)
Function Anti-ship missile
Manufacturer Lyme and Martens Industries
Design No. LMR-28
GSI No. GWS.52
Unit cost
ASM:
SSM, SLCM:

$1.38 million
$1.4 million
Service dates 2003-present
General characteristics
Length
ASM:
SSM, SLCM:
LC:

8 m
8.52 m
8.9 m
Diameter
Missile:
LC:

65 cm
70 cm
Finspan 75 cm
Wingspan 196 cm
Launch mass
AGM:
SSM, SLCM:

2500 kg
3000 kg
Launch canister
GWLS.39M, sub:
GWLS.35M2/3:

3800 kg
3942.53 kg
Flight characteristics
Propulsion
Stage 1:
Stage 2:

RBS.52 solid rocket booster
ATG-15R turbo-ramjet
Flight control Tail control fins, thrust vectoring
Speed Mach >3.22 max.
Manoeuvrability >12g
Range
AGM:
LC:

570 km
325 km
Ceiling 15 km
Guidance and payload
Guidance
Midcourse:

Terminal:

GPS/INS, AOSAM, command uplink
Dual-mode radar with IIR and automatic target recognition
Warhead BROACH APHE (300 kg)
Fuzes Timed penetrator, contact
Launch platforms
Ship GWLS.35M2-M3, GWLS.39, GWLS.58
Land L13/52
Operators
UKIN

The GWS.52 Pelican was developed by Lyme and Martens Industries to replace the GWS.39-3 Jewel (Yakhont 3) in domestic service.

The "Pelican," like the Pigeon is really a one-way drone with many advanced features allowing it to evade most missile defences as it approaches its targets. Like its siblings the Rook and the Tern, the "Pelican" possesses an effective autonomous operation situational awareness module (AOSAM) permitting the missile to alter its flight characteristics and use its minute radar cross-section and small infrared signature as well as active electronic countermeasures (ECM) to counter enemy threats as well as to respond to enemy countermeasures (ECCM), thus giving the "Pelican" a greater probability of successful strikes.

Like the GWS.39-3, the GWS.52 can work individually but is even deadlier in flocks. With its Link 17.2G secure data link, the lead "Pelican" operating at altitude can communicate with the other missiles in the flock to assign and prosecute targets ensuring a wider range of strikes against enemy ships. With this data link connection, the "Pelican" can receive targetting information from dedicated reconnaissance satellites, aerial vehicles providing over-the-horizon guidance, or from the firing vehicle. With this information, the GWS.52 can prosecute an enemy from various angles, regulating its thrust to ensure either a staggered or unique arrival time in the target zone. Furthermore, the data link permits attacks to be performed in conjunction with other combat drones, such as the "Puffin" or the "Rook," to minimise probability of intercept. For instance, the "Puffin" or "Rook" can use its search radar to illuminate the enemy fleet allowing the entire flock of "Pelicans" to remain below the enemy radar. Also, "Pelicans" and "Pigeons" can engage in a combined assault against a hostile fleet: the "Pigeons" eliminate the enemy's air defences while the "Pelicans" advance towards their targets.

Adding to the small EM signature of the "Pelican" is its ability to use either its small low-probability of intercept (LPI) radar or imaging infra-red sensors to home in on a specific target without revealing its presence.

When air launched from high altitude (10-15 km), the "Pelican" may initially proceed to target at 10-12 km altitude until its radar warning receivers begin detecting hostile emissions. The "Pelican" then descends to between 20 m and 5 m, or lower if sea states permit, and accelerates towards its targets. From about 50 km away, one missile (if in a flock) ascends to acquire targets and transmits this data to the other missiles as it descends. This hi-lo profile and the "Pelican's" supercruise turbo-ramjet engine allows a maximum range of 560 km. When either air launched from low altitude, or surface or submarine launched, the "Pelican" may opt for a lo-hi-lo attack profile, allowing attacks from as far away as 325 km. The "Pelican" may also perform a direct lo-lo assault. Using supercruise, the GWS.52 can prosecute targets from over 240 km distant, while operating at full speed (Mach 3+) the "Pelican" can travel up to 175 km to its prey.

All in all, the GWS.52 offers a great advance in the field of modern naval superiority.

GWS.52-1

Function: Supersonic cruise anti-ship missile (AShM)
Service designation:
Air: AGM.52A
Ground: FGM.52A
Sub-surface: UGM.52A
Surface ship: MGM.52A
Dimensions:
Length: 8 m (ASM); 8.52 m (SSM or SLCM)
Diameter: 60 cm (core)
Finspan (deployed): 75 cm
Wingspan (deployed): 1.96 m
Launch canister (LC):
—L13/52, GWLS.39M, or sub (cylindrical): 65 cm diameter; 890 cm high
—GWLS.35M2/M3 (l × w × h): 65 cm/70 cm × 65 cm/70 cm × 900 cm
Mass:
Air launched version: 2500 kg
Surface-/Submerged-launched version: 3000 kg (launch weight)
Launch canister:
—L13/52, GWLS.39M, or sub (loaded): 3800 kg
—GWLS.35M2/M3 (loaded): 3942.53 kg
Warhead: 250 kg APHE
Propulsion:
Booster: RBS.52
Missile: ATG-15R turbo-ramjet
Guidance:
Initial and midcourse: command datalink, AOSAM, and INS/GPS
Search: DRQ.52 LPI dual-mode radar with SAR; DAS.52 IIR; DEQ.8 ATR
Countermeasures: DRR.87 radar warning receiver system, DPR.6 laser warning receiver system, DSX.81 IFF
Launch Angle: Vertical to 15° from the horizontal, with 360° initial acquisition capability
Range (dependent on launch and attack profile):
Air launched, hi-lo attack: 570 km (max.)
Air, surface, or submarine launched, lo-hi-lo profile: 325 km (max.)
Surface or submarine launched, supercruise with full speed terminal (50+ km), lo-lo profile: 260 km (max.)
Surface or submarine launched, full speed, lo-lo profile: 175 km (max.)
Ceiling: 15 km; attack altitude 10-5 m and lower (depending on sea states)
Speed: Mach 1.65 (supercruise); Mach 3.22+ (terminal)
Cost: $1.225 million

GWS.52-2

Function: Supersonic cruise AShM
Service designation:
Air: AGM.52B
Ground: FGM.52B
Sub-surface: UGM.52B
Surface: MGM.52B
Dimensions:
Length: 8m (ASM), 8.52m (SSM)
Diameter: 60cm (core)
Finspan (ASM/deployed): 75cm
Wingspan (deployed): 1.96m
Launch canister (LC):
—L13/52, GWLS.39M, or sub (cylindrical): 65 cm diameter; 890 cm high
—GWLS.35M2/M3 (l × w × h): 65 cm/70 cm × 65 cm/70 cm × 943 cm
Mass:
Air-launched: 2500kg (2.5t)
Surface-/Submerged-launched: 3000 kg
Launch canister:
—L13/52, GWLS.39M, or sub (loaded): 3800 kg
—GWLS.35M2/M3 (loaded): 3942.53 kg
Warhead: 300 kg APHE
Propulsion:
Boosters: RBS.52B
Missile: ATG-15R2 turbo-ramjet
Guidance:
Initial and midcourse: command datalink, AOSAM, and INS/GPS
Search: LPI dual-mode radar with ISAR, IIR, ATR
Countermeasures: DRR.87B(V)2 radar warning receiver system, DPR.16B(V)2 laser warning receiver system, DSX.81 IFF
Launch Angle: Vertical to 15° from the horizontal, with 360° initial acquisition capability
Range:
Air launched, hi-lo attack: 600 km (max.)
Air, surface, or submarine-launched, lo-hi-lo profile: 350 km (max.)
Surface or submarine-launched, supercruise with full speed terminal (50+ km), lo-lo profile: 275 km (max.)
Surface or submarine-launched, full speed, lo-lo profile: 180 km (max.)
Ceiling: 15 km; attack altitude 10-5 m and lower (depending on sea states)
Speed: Mach >2.5 (cruise); Mach >3.22 (terminal)
Cost: (ASM): $1.38 million; (LC): $1.4 million

GWS.52-3

Function: Supersonic cruise AShM
Service designation:
Air: AGM.52C
Ground: FGM.52C
Sub-surface: UGM.52C
Surface: MGM.52C
Dimensions:
Length: tbd
Diameter: 60cm (core)
Finspan (ASM/deployed): 75cm
Wingspan (deployed): 1.96m
Launch canister (LC):
—L13/52, GWLS.39M, or sub (cylindrical): 65 cm diameter; 890 cm high
—GWLS.35M2/M3 (l × w × h): 65 cm/70 cm × 65 cm/70 cm × 943 cm
Mass:
AGM: tbd
FGM, MGM, UGM: tbd
Launch canister:
—GWLS.39M or sub (empty): 800 kg
—GWLS.35M2/M3 (empty): 942.53 kg
Warhead: tbd
Propulsion:
Boosters: RBS.52C (ASM); RBS.52D (other)
Missile: ATG-29J turbojet
Guidance:
Initial and midcourse: command datalink, AOSAM, and INS/GPS
Search: LPI dual-mode radar with ISAR, IIR, ATR
Countermeasures: Radar warning receiver system, laser warning receiver system, IFF
Launch Angle: Vertical to 15° from the horizontal, with 360° initial acquisition capability
Range (dependent on launch and attack profile):
Air launched, hi-lo attack: tbd
Air, surface, or submarine-launched, lo-hi-lo profile: tbd
Surface or submarine-launched, supercruise with full speed terminal (50+ km), lo-lo profile: tbd
Surface or submarine-launched, full speed, lo-lo profile: tbd
Ceiling: >26 km
Speed: Mach 3.77 (max., 11-25 km altitude), Mach 3.22 (terminal, diving), Mach 3.07 (ASL)
Cost: tbd


Surface-to-surface missiles
Ahab | Battle Axe | Doomsday | Hájord | Hatchet | Hurricane | Jupiter | HyStrike | Khan | Pelican | Sicarius | Starbolt | Stryker | Vidofnir | Yakhont 3


Isselmere-Nieland Defence Industries
DAS | IMW | LMI | RINO | RSIN

Aircraft:
Angrboda | Cormorant | Gargantua | Garuda | Pantagruel | Scimitar | Sea Fury | Sparrow | Spectre | Swordfish | Tiger
Countermeasures and Decoys:
Flamingo
Ground Vehicles:
L15 LAV series | L21 HAV series | L25 Boar SPH | Lion | Mammoth OCV
Launchers:
GWLS.35 | GWLS.58 | GWLS.60
Missiles and Torpedoes:
Ahab | Barracuda | Erne | Hurricane | Loon | Mako | Pelican | Sailfish | Triton | Vidofnir
Small Arms and Crew-Served Weapons:
L117 | L118 | L119 | L120
Uncrewed Vehicles:
Albatross | Auk/Puffin | Canary | Clownfish | Cuttlefish | Dodo | Dolphin | Ferret | Horus | Hyena | Iguana | Jackal
Marmot | Mule | Parrot | Penguin | Pike | Porpoise | Rook | Seahorse | Squid | Tern | Thrush | Wyvern | Urchin
Vessels:
Bullfinch | City (2003) | City (2007) | County (2003) | Crocodile | Europa | Flower (2005) | Furtive | Grand Duchy | King Henry V | King Robert VI
Kingdom (2005) | Lethe | Lord | Marquess | Province (2003) | River (2003) | Royal Edmund | Síanach | Town (2007) | Union | Wallace
Other Equipment:
AOSAM | ISOMS | KERI foam | MITRE | MUSE | NAIADS | ODIN | SELKIE | SPINTOP


UKIN banner vsm.jpg Topics on Isselmere-Nieland UKIN banner vsm.jpg
Category | Factbook

Categories: Administrative divisions | Constitution | Defence Forces | Festivities | Government | Languages | Laws
Subjects: Capital | Coat of arms | Currency | Economy | Education | Football | History | Lethean Islands | Religion
Monarchy: History | Royal Family
Government: Council of State | DPA | Lords Commissioners | The King | Parliament | Prime Minister | Storting of Nieland
Firms: Detmerian Aerospace | Isselmere Motor Works | Lyme and Martens | Royal Ordnance | Royal Shipyards | Turing-Babbage | UPGO
Products: Isselmere-Nieland Defence Industries