Current Year
2789 A.D.
Arms of Humanity
Infantry Arms
Sidebar
armaments:human:rocketsandmissiles:naja_missile
Stanley-Vought GIM-52 'Naja' Long Range Missile
General Information and Design Details
A
Sensors and Guidance
- EG/EQR-72M8 Micro AESA Radar Array
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
Service and Production History
In Service
2752 A.D.
Production Began
2715 A.D.
Manufacturer
Stanley-Vought of the United American Systems
Statistics and Information
Mass
1,155 kg (2,546 lbs)
Diameter
39.8 CM (15.7 IN)
Drive System
Douglas-Hughes GJ3-575M
A-MAT Augmented Pulsed Fusion Drive
Propellant
Solid Lithium-7 Deuteride Fusion Motor / Anti-Hydrogen 'Bottle'
Burn Time
4 Minutes of Drive Impulse (Capable of ~2000 G Acceleration)
Average Velocity (In Vacuum)
3.25% C (Terminal Attack)
1.85% C (Coasting / Search-Acquire-Track)
Average Engagement Envelope
Normal
1.5 to 4 Light Seconds
Standoff
0.5 to 1.0 Light Minutes
armaments/human/rocketsandmissiles/naja_missile.txt · Last modified: 2026/05/05 04:48 by arieg203
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