GSM.38 Jupiter ASM

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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 7
Terminal Stage: Mach 11
Manoeuvrability >16g
Range 4,350NM
Ceiling 110km
Guidance and payload
Guidance Midcourse:

Terminal:

  • Dual-mode radar with IIR
  • CIP with Optronics
  • LADAR/LIDAR
  • 10m CEP.
Warhead
  • 1.6 Ton DU Penetrator with 3,100kg PulseWave Propellant
  • 5,800kg High-Explosive Warhead
Fuzes Timed penetrator, contact, airburst.
Launch platforms
Ship
Land
Operators
Artitsan Imperial Navy | Artitsan Imperial Airforce


GSM.38 Jupiter Heavy Anti-Shipping Missile

Design and Testing

The GSM.38 is known to have been requested as early as 1997, as a competitor to the Khan Class Missile developed by ZMI. The missile is quite similar in specifications, with the GSM.38 being slightly larger, only to match Artitsan VLS standards. The missile is designed for the same role; To devestate enemy capital and super capital vessels in a single shot. The ability to directly compare it to the Khan has allowed improvements in several aspects including range, survivability, killing power, and Intelligence.

Propulsion

The GSM.38 uses several seperate propulsion systems built by the renowned Nolan-Petyav Aerospace Propulsion Industries. These engines are incredibly advanced in comparison, allowing for better Fuel Effeciency and performance, increasing both range and velocity.

Stage 1: This cold launch system allows for rapid deployment, and prevents any thermal damage to surrounding structures. Designed to simply push the missile up and away from its launch platform. Stage 2: Used to propel the missle to an altitude which would allow the RAMjet to perform effectively. Stage 3: The rocket uses a pulse-detonation system to achieve an appropriate speed for the RAMjet to kick in. This stage is used for the majority of the flight time. Stage 4: The terminal phase, the SCRAMjet achieves an incredibly high-speed before dropping too low to the surface, when the Pulse-Detonation system kicks in.

Attack Profile

Hi-Hi-Lo prawnage

Counter-Measures

Stuff liek jammers and stuff.


Surface-to-surface missiles
Ahab | Battle Axe | Doomsday | Hájord | Hatchet | Hurricane | Jupiter | HyStrike | Khan | Pelican | Sicarius | Starbolt | Stryker | Vidofnir | Yakhont 3