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2889 A.D.

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xover:technologies:military:confedmissiles:peacemaker_missile

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S/LGM-118 ‘Peacemaker’ Interstellar Bombardment Missile (ISBM)

General Information and Design Details

A

Sensors and Guidance

  • High Gain Hyperspectral Optical Sensor
    A

Control System

  • 'Brilliant' Class Guided Munition
    A

Payload

  • Robust Terrestrial Penetration Warhead (RTP) (MOD 1)
    A

  • KADAM Warhead (MOD 2)
    A

  • ADAM Warhead (MOD 3)
    A

  • Flechette 'Hornet' Warhead (MOD 4)
    A

Countermeasures / Decoys

  • Thermal Maneuvering Decoy Ballutes
    A

  • Active Maneuvering Submunitions
    A

Service and Production History

In Service
2615 A.D.

Production Began
2602 A.D.

Manufacturer
Stanley-Vought of the United American Systems

Statistics and Information

Mass
422 Tonnes

Diameter
10.2 M (33.46 FT)

Drive System
Douglas-Hughes SPU-120
A-MAT Augmented Pulsed Fusion Drive


Stanley-Vought XCM-520
Consumable FTL Jump Drive


Propellant
Solid Lithium-7 Deuteride Fusion Motor / Anti-Hydrogen 'Bottle'

Burn Time
600 Minutes of Drive Impulse (Capable of ~2000 G Acceleration)

Average Velocity (In Vacuum)
1.5% C (Terminal Attack)
1.15% C (Coasting / Search-Acquire-Track)

Range
1,250 Light Years

See Also


xover/technologies/military/confedmissiles/peacemaker_missile.1769936189.txt.gz · Last modified: 2026/02/01 08:56 by arieg203