Difference between revisions of "GWS.64 Mako"
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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; " | ||
+ | |- 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 | Mako | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Design details (GWS.64-2) | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Function | ||
+ | |[[Wikipedia:Torpedo|Torpedo]] | ||
+ | |- 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.]] | ||
+ | |LMT-2 | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Defence Procurement Agency (Isselmere-Nieland)#61-80|DPA No.]] | ||
+ | |GWS.64 | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Currency|Unit cost]] | ||
+ | |$1.38 million ([[Wikipedia:Air-to-surface_missile|ASM]])<br>$1.4 million ([[Wikipedia:Surface-to-surface_missile|SSM]] or [[Wikipedia:SLCM|SLCM]]) | ||
+ | |- 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; font-weight:bold;"| Length | ||
+ | | 8 m (ASM)<br>8.52 m (SSM or SLCM)<br>8.9 m (LC) | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Diameter | ||
+ | | 65 cm (ASM,SLCM)<br>70 cm (SSM) | ||
+ | |- | ||
+ | |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; font-weight:bold;"| Launch mass | ||
+ | | 2500 kg (AGM)<br>3000 kg (other) | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Launch canister | ||
+ | | 3800 kg (GWLS.39M, sub)<br>3942.53 kg (GWLS.35M2/3) | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Flight characteristics | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion | ||
+ | |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]] >3.22 max. | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability | ||
+ | |>12''[[Wikipedia:Acceleration_due_to_gravity|g]]'' | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Range | ||
+ | |570 km (AGM)<br>325 km (LC) | ||
+ | |- 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; font-weight:bold;"|Guidance | ||
+ | |'''Midcourse:''' | ||
+ | *[[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="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Warhead|Warhead]] | ||
+ | |APHE (310 kg) | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Fuzes | ||
+ | |Hydrostatic pressure, impact | ||
+ | |- | ||
+ | ! 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]] | ||
+ | |21" (533mm) torpedo tube | ||
+ | |- | ||
+ | ! 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.64 Mako''' is the primary heavyweight torpedo ('''HWT''') in service with the [[Royal Isselmere-Nieland Navy]] for general purpose anti-submarine and anti-ship warfare. The torpedo has a body diameter of 21 inches so may be fired by most submarines. | The '''GWS.64 Mako''' is the primary heavyweight torpedo ('''HWT''') in service with the [[Royal Isselmere-Nieland Navy]] for general purpose anti-submarine and anti-ship warfare. The torpedo has a body diameter of 21 inches so may be fired by most submarines. | ||
Revision as of 03:03, 19 June 2007
Profile (n/a) | |
Mako | |
---|---|
Design details (GWS.64-2) | |
Function | Torpedo |
Manufacturer | Lyme and Martens Industries |
Design No. | LMT-2 |
DPA No. | GWS.64 |
Unit cost | $1.38 million (ASM) $1.4 million (SSM or SLCM) |
Service dates | 2003-present |
General characteristics | |
Length | 8 m (ASM) 8.52 m (SSM or SLCM) 8.9 m (LC) |
Diameter | 65 cm (ASM,SLCM) 70 cm (SSM) |
Finspan | 75 cm |
Wingspan | 196 cm |
Launch mass | 2500 kg (AGM) 3000 kg (other) |
Launch canister | 3800 kg (GWLS.39M, sub) 3942.53 kg (GWLS.35M2/3) |
Flight characteristics | |
Propulsion | RBS.52 solid rocket booster ATG-15R turbo-ramjet |
Flight control | Tail control fins, thrust vectoring |
Speed | Mach >3.22 max. |
Manoeuvrability | >12g |
Range | 570 km (AGM) 325 km (LC) |
Ceiling | 15 km |
Guidance and payload | |
Guidance | Midcourse:
Terminal: |
Warhead | APHE (310 kg) |
Fuzes | Hydrostatic pressure, impact |
Launch platforms | |
Ship | 21" (533mm) torpedo tube |
Operators | |
UKIN |
The GWS.64 Mako is the primary heavyweight torpedo (HWT) in service with the Royal Isselmere-Nieland Navy for general purpose anti-submarine and anti-ship warfare. The torpedo has a body diameter of 21 inches so may be fired by most submarines.
GWS.64-1
Function: heavyweight general-purpose torpedo
Dimensions: length: 6.05m; diameter: 533mm
Mass: 1737.42 kg; warhead: 305.6 kg (U2: 310 kg) shape-charged directional APHE
Propulsion: hydrogen ammonium perchlorate and Otto II (HAP-Otto) fueled open-cycle gas turbine driving a pump-jet propulsor
Guidance: primary: fibre-optic wire-guided, active/passive sonar with laser INS and AOSAM; reacquisition and terminal: wake homing
Fuzing: hydrostatic proximity or impact
Range: ~30 km (68 kts.), 54 km (50 kts.)
Depth: minimum standard operating depth: >25m; maximum operating depth: 1,500m
Speed: 70 kts. maximum
Cost: $2.5 million
GWS.64-2
Function: heavyweight general-purpose torpedo
Dimensions: length: 6.2m; diameter: 533mm
Mass: 1848.34 kg; warhead: 310 kg shape-charged directional APHE
Propulsion: hydrogen ammonium perchlorate and Otto II (HAP-Otto) fueled open-cycle gas turbine driving a pump-jet propulsor
Guidance: primary: fibre-optic wire-guided, active/passive sonar with laser INS and AOSAM; reacquisition and terminal: wake homing
Fuzing: hydrostatic proximity or impact
Range: 40 km (80 kts.), 67 km (50 kts.)
Depth: minimum standard operating depth: >25m; maximum operating depth: 1,500m
Speed: 80+ kts. maximum
Cost: $2.85 million
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