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Specification
Antares 130
Orbital Sciences Corporation
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Proton K/DM-2
Khrunichev State Research and Production Space Center
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Flights
1
110
Success rate
0%
93.6%
Thrust
3,265 kN
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Height
41.9 m
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Diameter
3.9 m
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Launch mass
286 t
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LEO capacity
5,100 kg
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GTO capacity
—
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Launch cost
—
—
Reusable
No
No
Stages
2
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