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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

  • FISLE Warhead (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
2701 A.D.

Production Began
2710 A.D.

Manufacturer
Douglas-Hughes of the United American Systems

Statistics and Information

Mass
2,725 kg (6007 lbs)

Diameter
63.5 CM (25 IN)

Drive System
Douglas-Hughes SPU-082
A-MAT Augmented Pulsed Fusion Drive


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

Burn Time
8 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)

Average Engagement Envelope
Normal
0.5 to 2 Light Seconds
Standoff
0.8 to 1.8 Astronomical Units

See Also


xover/technologies/military/confedmissiles/peacemaker_missile.1769934936.txt.gz · Last modified: 2026/02/01 08:35 by arieg203