Difference between revisions of "GSM.38 Jupiter ASM"
From NSwiki, the NationStates encyclopedia.
Line 1: | Line 1: | ||
+ | {| 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 |http://www.nationstates.net/images/flags/uploads/artitsa.jpg | ||
+ | |-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 | Jupiter | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Design details (GSM.38) | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Function | ||
+ | |[[Wikipedia:Air-to-surface_missile|ASM]], [[Wikipedia:Surface-to-surface_missile|SSM]], [[Wikipedia:SLCM|SLCM]] | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Manufacturer | ||
+ | |[[TBA]] | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Design No. | ||
+ | |PASM-91 | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold|- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Currency|Unit cost]] | ||
+ | |$191 Million<br> | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Service dates | ||
+ | |[[Wikipedia:2006|2006]]-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 | ||
+ | | | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Diameter | ||
+ | | | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Finspan | ||
+ | | | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Wingspan | ||
+ | | | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"| Launch mass | ||
+ | | | ||
+ | |- | ||
+ | ! 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="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control | ||
+ | | | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Speed | ||
+ | | | ||
+ | |- 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 | ||
+ | | | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|Ceiling | ||
+ | | | ||
+ | |- | ||
+ | ! 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]] | ||
+ | |500 kg BROACH APHE | ||
+ | |- | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Fuze|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.58 missile launch system|GWLS.58]] | ||
+ | |- style="background:#f0f0f0;" | ||
+ | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Army|Land]] | ||
+ | |L13/58 | ||
+ | |- | ||
+ | ! colspan=2 style="text-align:center; font-weight:bold; background:#99ccff;" | Operators | ||
+ | |- | ||
+ | |colspan=2 style="vertical-align:top; text-align:center;"|[[Isselmere-Nieland|UKIN]] | ||
+ | |} | ||
+ | |||
+ | |||
==GSM.38 Jupiter Heavy Anti-Shipping Missile== | ==GSM.38 Jupiter Heavy Anti-Shipping Missile== | ||
Revision as of 20:15, 6 June 2007
Profile (n/a) | ||
Jupiter | ||
---|---|---|
Design details (GSM.38) | ||
Function | ASM, SSM, SLCM | |
Manufacturer | TBA | |
Design No. | PASM-91 | |
- | Unit cost | $191 Million |
Service dates | 2006-present | |
General characteristics | ||
Length | ||
Diameter | ||
Finspan | ||
Wingspan | ||
Launch mass | ||
Flight characteristics | ||
Propulsion | ||
Flight control | ||
Speed | ||
Manoeuvrability | >12g | |
Range | ||
Ceiling | ||
Guidance and payload | ||
Guidance | Midcourse:
Terminal: | |
Warhead | 500 kg BROACH APHE | |
Fuzes | Timed penetrator, contact | |
Launch platforms | ||
Ship | GWLS.58 | |
Land | L13/58 | |
Operators | ||
UKIN |
GSM.38 Jupiter Heavy Anti-Shipping Missile
Ahab | Battle Axe | Doomsday | Hájord | Hatchet | Hurricane | Jupiter | HyStrike | Khan | Pelican | Sicarius | Starbolt | Stryker | Vidofnir | Yakhont 3 |