Difference between revisions of "GSM.38 Jupiter ASM"
From NSwiki, the NationStates encyclopedia.
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|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion | |style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion | ||
− | |NP-M-65 Rocket | + | |NP-R-03 Cold Rocket Booster<br>NP-M-65 Rocket Engine<br>NP-139H RAMjet Booster to PDE<br>NP-M-127 SCRAMjet/PDE |
|- 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 | ||
− | + | |Mission Adaptive Skin<br>Forward Thrust Nozzels<br>Active-Aeroelastic Wings<br>45* 3D Thrust Vectoring<br>Rotating Canards | |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Speed | |style="vertical-align:top; text-align:right; font-weight:bold;"|Speed | ||
− | | | + | |First Stage: Mach 2+<br>Second Stage: Mach 3.5<br>Third Stage: Mach 6<br>Terminal Stage: Mach 9 to 11 |
|- style="background:#f0f0f0;" | |- style="background:#f0f0f0;" | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability | |style="vertical-align:top; text-align:right; font-weight:bold;"|Manoeuvrability | ||
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|- | |- | ||
! 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 | ||
+ | |Osmium Penetrator | ||
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|Guidance | |style="vertical-align:top; text-align:right; font-weight:bold;"|Guidance | ||
|'''Midcourse:''' | |'''Midcourse:''' | ||
− | *[[Wikipedia:Global_Positioning_System|GPS]]/[[Wikipedia:Inertial_guidance_system| | + | *[[Wikipedia:Global_Positioning_System|GPS]]/[[Wikipedia:Inertial_guidance_system|Inertial Guidance]], command uplink |
'''Terminal:''' | '''Terminal:''' | ||
*Dual-mode [[Wikipedia:Radar|radar]] with [[Wikipedia:Imaging_infrared|IIR]] and automatic target recognition | *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]] | ||
− | | | + | |BokBokBok |
|- | |- | ||
|style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Fuze|Fuzes]] | |style="vertical-align:top; text-align:right; font-weight:bold;"|[[Wikipedia:Fuze|Fuzes]] |
Revision as of 13:45, 7 June 2007
Profile (n/a) | ||
Jupiter | ||
---|---|---|
Design details (GSM.38) | ||
Function | ASM, SSM, SLCM | |
Manufacturer | Harker-Boss Precision Rocketry | |
Design No. | PASM-91 | |
Unit cost | $134 Million | |
Service dates | 2006-present | |
General characteristics | ||
Length | 25.2m | |
Diameter | 2.6m | |
Finspan | Not Released | |
Wingspan | Not Released | |
Launch mass | 96 Tons | |
Flight characteristics | ||
Propulsion | NP-R-03 Cold Rocket Booster NP-M-65 Rocket Engine NP-139H RAMjet Booster to PDE NP-M-127 SCRAMjet/PDE | |
Flight control | Mission Adaptive Skin Forward Thrust Nozzels Active-Aeroelastic Wings 45* 3D Thrust Vectoring Rotating Canards | |
Speed | First Stage: Mach 2+ Second Stage: Mach 3.5 Third Stage: Mach 6 Terminal Stage: Mach 9 to 11 | |
Manoeuvrability | >12g | |
Range | ||
Ceiling | ||
Guidance and payload | Osmium Penetrator | |
Guidance | Midcourse:
Terminal: | |
Warhead | BokBokBok | |
Fuzes | Timed penetrator, contact | |
Launch platforms | ||
Ship | ||
Land | ||
Operators | ||
Artitsan Imperial Navy | Artitsan Imperial Airforce |
GSM.38 Jupiter Heavy Anti-Shipping Missile
Ahab | Battle Axe | Doomsday | Hájord | Hatchet | Hurricane | Jupiter | HyStrike | Khan | Pelican | Sicarius | Starbolt | Stryker | Vidofnir | Yakhont 3 |