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SF-3A Lancer II

 

sf-3a

 

General and Technical Data

 

Model number: SF-3A
Code name: Lancer II
Unit type: mass production space fighter
Manufacturer: Lockhee
Operator: U.N. Spacy

Rollout: unknown
First deployment: March AD 2009
Accommodation: pilot only, in standard cockpit
Dimensions: overall height 2.65 meters; overall length 13.2 meters
Weight: empty 9.5 metric tons; standard takeoff mass 15.7 metric tons
Armor materials: unknown
Powerplant: OTEC thermonuclear reaction rocket engine, power output rating unknown
Propulsion: 153000 kg for 60 seconds (1500.93 kN); 230000 kg for 5 seconds (2256.3 kN); vernier belt, mounted in nose; high maneuverability vernier, mounted in rear

Performance: maximum speed 7.0 km/s
Equipment and design features: movable targeting radar antenna, sensor range unknown, mounted on dorsal fuselage, targeting camera, mounted on nose
Fixed armaments: 2 x Howard long-range charged particle beam cannon, output rated at 750 MW each, mounted on forward section; 2 x Hughes anti-aircraft thermonuclear reaction missile, 0.5 kiloton class yield, mounted on rear fuselage

 

Technical and Historical Notes

 

The SF-3A Lancer II was a space fighter manufactured by Lockhee for use by U.N. Spacy. This interceptor craft was deployed to ships like the ARMD class space carriers. Equipped with an OverTechnology reaction rocket engine, the Lancer was designed for high speed attacks. Its armaments included two Howard long-range charged particle beam cannons, as well as two Hughes anti-aircraft reaction missiles. Lancers were among the first U.N. Spacy craft to engage the Zentradi forces in space at the start of Space War I in February 2009.

 

Miscellaneous Information

 

Appearances: Super Dimension Fortress Macross (TV series)
Original mechanical designer: Kazutaka Miyatake

 

Lineart

 

Thermonuclear reaction missile

 

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