Difference between revisions of "GWS.82 Triton"

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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; "
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|- style="background:#f0f0f0; text-align:center; width=250px;"
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| align=center colspan=2 |http://www.nationstates.net/images/flags/kiribati--53.jpg
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|-style="background:#f0f0f0;"
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| align=center colspan=2 | '''Profile (n/a)'''
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|- style="text-align:center; background:#f0f0f0;"
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| colspan=2 style="padding:0; background:#996; color:#fff;" |
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|- style="color:#fff; background:#69c; font-size:140%;"
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! colspan=2 | Triton
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|-
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! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Design details
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"| Function
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|[[Wikipedia:Air-to-surface_missile|Air-to-surface]] or [[Wikipedia:Surface-to-surface_missile|surface-to-surface missile]]
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Manufacturer
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|[[Lyme and Martens Industries]]
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Design No.
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|LMR-61
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Defence Procurement Agency (Isselmere-Nieland)#81-100|DPA No.]]
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|GWS.82
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Currency|Unit cost]]
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|$65 million
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates
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|[[Wikipedia:2005|2005]]-present
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|-
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! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |General characteristics
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"| Length
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|17.22 m
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"| Diameter
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|2.7 cm (Core/LC)
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"| Launch mass
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| 122.92 t
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|-
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! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Flight characteristics
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion
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|RSS.82A1 solid rocket<br>RSS.82A2 solid rocket<br>RSS.82A3 solid rocket
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control
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|Thrust vectoring
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Speed
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|&gt;29000 km/h
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability
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|''[[Wikipedia:Acceleration_due_to_gravity|g]]''
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Range
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|&gt;12000 km
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling
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|Low Earth orbit
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|-
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! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" |Guidance and payload
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Guidance
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|'''Initial:'''
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*[[Wikipedia:Global_Positioning_System|GPS]]/[[Wikipedia:Inertial_guidance_system|INS]]
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'''Midcourse:'''
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*GPS/INS, celestial reference
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'''Terminal:'''
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*Dual-mode GPS/INS and ATR
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|- style="background:#f0f0f0;"
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|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Warhead|Warhead]]
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|8 &times; 950 kt warheads
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|Fuzes
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|Barometric/RF altimeter, contact
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|-
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! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Launch platforms
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|-
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|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Navy|Ship]]
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|GWLS.82
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|-
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! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Operators
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|-
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|colspan=2 style="vertical-align:top; text-align:center;"|[[Isselmere-Nieland|UKIN]]
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|}
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A [[Wikipedia:Submarine-launched_ballistic_missile|submarine-launched ballistic missile]] ('''SLBM''') designed to replace the smaller [[Wikipedia:Trident_SLBM|UGM-133A Trident D5]] aboard the [[Chamberlain-class SSBN|Chamberlain-class]] [[Wikipedia:Ballistic_missile_submarine|ballistic missile submarines]].
 
A [[Wikipedia:Submarine-launched_ballistic_missile|submarine-launched ballistic missile]] ('''SLBM''') designed to replace the smaller [[Wikipedia:Trident_SLBM|UGM-133A Trident D5]] aboard the [[Chamberlain-class SSBN|Chamberlain-class]] [[Wikipedia:Ballistic_missile_submarine|ballistic missile submarines]].
  

Revision as of 21:16, 29 July 2006

kiribati--53.jpg
Profile (n/a)
Triton
Design details
Function Air-to-surface or surface-to-surface missile
Manufacturer Lyme and Martens Industries
Design No. LMR-61
DPA No. GWS.82
Unit cost $65 million
Service dates 2005-present
General characteristics
Length 17.22 m
Diameter 2.7 cm (Core/LC)
Launch mass 122.92 t
Flight characteristics
Propulsion RSS.82A1 solid rocket
RSS.82A2 solid rocket
RSS.82A3 solid rocket
Flight control Thrust vectoring
Speed >29000 km/h
Manoeuvrability g
Range >12000 km
Ceiling Low Earth orbit
Guidance and payload
Guidance Initial:

Midcourse:

  • GPS/INS, celestial reference

Terminal:

  • Dual-mode GPS/INS and ATR
Warhead 8 × 950 kt warheads
Fuzes Barometric/RF altimeter, contact
Launch platforms
Ship GWLS.82
Operators
UKIN

A submarine-launched ballistic missile (SLBM) designed to replace the smaller UGM-133A Trident D5 aboard the Chamberlain-class ballistic missile submarines.

GWS.82U

Types:
Submarine launched ballistic missile (SLBM)
Anti-satellite weapon launching system (ASAT)
Satellite launching system (SAT-L)
Service designation:
SLBM: UGM.82
ASAT: UIM.82
SAT-L: UCM.82
Dimensions:
Length: 17.22 m
Diameter: 2.7 m
Mass: 122920 kg
Warhead: SLBM: 16 × W88 (475 kt) multiple independently targetable re-entry vehicles (MIRV) or 16 × W76 (100 kt)
Payload: 5880 kg
Propulsion: three-stage solid-propellant rocket, thrust-vector control for course corrections
Guidance:
Initial: inertial navigation corrected by global positioning satellite information (GPS)
Midcourse: inertial navigation corrected by celestial reference navigation system (CRNS)
Terminal: inertial navigation corrected by stored map reference guidance and GPS information.
Range: >12000 km
Cost: $65 million


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

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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

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