View source for GWS.52 Pelican

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|- style="background:#f0f0f0; text-align:center; width=250px;"
| align=center colspan=2 |[[Image:UKIN_banner.gif]]
|-style="background:#f0f0f0;"
| align=center colspan=2 | '''Profile (n/a)'''
|- style="text-align:center; background:#f0f0f0;"
| colspan=2 style="padding:0; background:#996; color:#fff;" |
|- style="color:#fff; background:#69c; font-size:140%;"
! colspan=2 | Pelican
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Design details (GWS.52-2)
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"| Function
|[[Wikipedia:Anti-ship_missile|Anti-ship missile]]
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[:Category:Corporations|Manufacturer]]
|[[Lyme and Martens Industries]]
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Lyme and Martens Industries|Design No.]]
|LMR-28
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Defence Procurement Agency (Isselmere-Nieland)#41-60|GSI No.]]
|GWS.52
|-
|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]]:
|<br>$1.38 million<br>$1.4 million
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates
|[[Wikipedia:2003|2003]]-present
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |General characteristics
|-
|style="vertical-align:top; text-align:right;"|'''Length'''<br>ASM:<br>SSM, SLCM:<br>LC:
|<br>8 m<br>8.52 m<br>8.9 m
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right;"|'''Diameter'''<br>Missile:<br>LC:
|<br>65 cm<br>70 cm
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|Finspan
|75 cm
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|Wingspan
|196 cm
|-
|style="vertical-align:top; text-align:right;"|'''Launch mass'''<br>AGM:<br>SSM, SLCM:
|<br>2500 kg<br>3000 kg
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right;"|'''Launch canister'''<br>GWLS.39M, sub:<br>GWLS.35M2/3:
|<br>3800 kg<br>3942.53 kg
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Flight characteristics
|-
|style="vertical-align:top; text-align:right;"|'''Propulsion'''<br>Stage 1:<br>Stage 2:
|<br>RBS.52 solid rocket booster<br>ATG-15R turbo-ramjet
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control
|Tail control fins, thrust vectoring
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|Speed
|[[Wikipedia:Mach|Mach]] &gt;3.22 max.
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability
|&gt;12''[[Wikipedia:Acceleration_due_to_gravity|g]]''
|-
|style="vertical-align:top; text-align:right;"|'''Range'''<br>AGM:<br>LC:
|<br>570 km<br>325 km
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling
|15 km
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Guidance and payload
|-
|style="vertical-align:top; text-align:right;"|'''Guidance'''<br>Midcourse:<br><br>Terminal:
|<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
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Warhead|Warhead]]
|BROACH APHE (300 kg)
|-
|style="vertical-align:top; text-align:right; font-weight:bold;"|Fuzes
|Timed penetrator, contact
|-
! 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]]
|[[GWLS.35 missile launch system|GWLS.35M2-M3]], GWLS.39, [[GWLS.58 missile launch system|GWLS.58]]
|- style="background:#f0f0f0;"
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Army|Land]]
|L13/52
|-
! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Operators
|-
|colspan=2 style="vertical-align:top; text-align:center;"|[[Isselmere-Nieland|UKIN]]
|}

The '''GWS.52 Pelican''' was developed by [[Lyme and Martens Industries]] to replace the [[Defence Procurement Agency (Isselmere-Nieland)#21-40|GWS.39-3 Jewel]] ([[Yakhont 3]]) in domestic service.

The "Pelican," like the [[GWS.50 Pigeon|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 [[LMI-3 Rook|Rook]] and the [[LMI-4 Tern|Tern]], the "Pelican" possesses an effective [[Autonomous Operation Situational Awareness Module|autonomous operation situational awareness module]] ('''AOSAM''') permitting the missile to alter its flight characteristics and use its minute radar cross-section and small [[Wikipedia:Infrared|infrared]] signature as well as active [[Wikipedia:Electronic_countermeasures|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 [[Wikipedia:Anti-ship_missile|anti-ship missile]] ('''AShM''')<br>
'''Service designation:'''<br>
Air: AGM.52A<br>
Ground: FGM.52A<br>
Sub-surface: UGM.52A<br>
Surface ship: MGM.52A<br>
'''Dimensions:'''<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: 60 cm (core)<br>
Finspan (deployed): 75 cm<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>
Air launched version: 2500 kg<br>
Surface-/Submerged-launched version: 3000 kg (launch weight)<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>
'''Propulsion:'''<br>
Booster: RBS.52<br>
Missile: ATG-15R turbo-ramjet<br>
'''Guidance:'''<br>
Initial and midcourse: command datalink, AOSAM, and INS/GPS<br>
Search: DRQ.52 LPI [[Wikipedia:Active_radar_homing|dual-mode radar]] with [[Wikipedia:Synthetic_aperture_radar|SAR]]; DAS.52 [[Wikipedia:Infrared_homing|IIR]]; DEQ.8 ATR<br>
'''Countermeasures:''' DRR.87 radar warning receiver system, DPR.6 laser warning receiver system, DSX.81 IFF<br>
'''Launch Angle:''' Vertical to 15° from the horizontal, with 360° initial acquisition capability<br>
'''Range (dependent on launch and attack profile):'''<br>
Air launched, hi-lo attack: 570 km (max.)<br>
Air, surface, or submarine launched, lo-hi-lo profile: 325 km (max.)<br>
Surface or submarine launched, supercruise with full speed terminal (50+ km), lo-lo profile: 260 km (max.)<br>
Surface or submarine launched, full speed, lo-lo profile: 175 km (max.)<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>
'''Cost:''' $1.225 million

==GWS.52-2==
'''Function:''' Supersonic cruise AShM<br>
'''Service designation:'''<br>
Air: AGM.52B<br>
Ground: FGM.52B<br>
Sub-surface: UGM.52B<br>
Surface: MGM.52B<br>
'''Dimensions:'''<br>
Length: 8m (ASM), 8.52m (SSM)<br>
Diameter: 60cm (core)<br>
Finspan (ASM/deployed): 75cm<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>
Air-launched: 2500kg (2.5t)<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>
'''Propulsion:'''<br>
Boosters: RBS.52B<br>
Missile: ATG-15R2 turbo-ramjet<br>
'''Guidance:'''<br>
Initial and midcourse: command datalink, AOSAM, and INS/GPS<br>
Search: LPI dual-mode radar with [[Wikipedia:Inverse_synthetic_aperture_radar|ISAR]], IIR, ATR<br>
'''Countermeasures:''' DRR.87B(V)2 radar warning receiver system, DPR.16B(V)2 laser warning receiver system, DSX.81 IFF<br>
'''Launch Angle:''' Vertical to 15° from the horizontal, with 360° initial acquisition capability<br>
'''Range:'''<br>
Air launched, hi-lo attack: 600 km (max.)<br>
Air, surface, or [[Wikipedia:SLCM|submarine-launched]], lo-hi-lo profile: 350 km (max.)<br>
Surface or submarine-launched, supercruise with full speed terminal (50+ km), lo-lo profile: 275 km (max.)<br>
Surface or submarine-launched, full speed, lo-lo profile: 180 km (max.)<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>
'''Cost:''' (ASM): $1.38 million; (LC): $1.4 million

==GWS.52-3==
'''Function:''' Supersonic cruise AShM<br>
'''Service designation:'''<br>
Air: AGM.52C<br>
Ground: FGM.52C<br>
Sub-surface: UGM.52C<br>
Surface: MGM.52C<br>
'''Dimensions:'''<br>
Length: ''tbd''<br>
Diameter: 60cm (core)<br>
Finspan (ASM/deployed): 75cm<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>
AGM: ''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>
'''Propulsion:'''<br>
Boosters: RBS.52C (ASM); RBS.52D (other)<br>
Missile: ATG-29J turbojet<br>
'''Guidance:'''<br>
Initial and midcourse: command datalink, AOSAM, and INS/GPS<br>
Search: LPI dual-mode radar with ISAR, IIR, ATR<br>
'''Countermeasures:''' Radar warning receiver system, laser warning receiver system, IFF<br>
'''Launch Angle:''' Vertical to 15° from the horizontal, with 360° initial acquisition capability<br>
'''Range (dependent on launch and attack profile):'''<br>
Air launched, hi-lo attack: ''tbd''<br>
Air, surface, or [[Wikipedia:SLCM|submarine-launched]], lo-hi-lo profile: ''tbd''<br>
Surface or submarine-launched, supercruise with full speed terminal (50+ km), lo-lo profile: ''tbd''<br>
Surface or submarine-launched, full speed, lo-lo profile: ''tbd''<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>
'''Cost:''' ''tbd''

{{Surface-to-surface missiles}}
{{Isselmere-Nieland Defence Industries}}
{{Isselmere-Nieland}}