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10 m20 m30 m35 mDelta III 8930
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Figure
Delta III 8930 US Air Force ✕
Size
Height 35.0 m
Diameter 4.0 m
Stages 2
Launch mass 301 t
Performance
First-stage engines 1 × RS-27A
Boosters 9 × GEM 46
Propellant LOX / RP-1
Thrust at liftoff 4,856 kN est.
Thrust-to-weight 1.64 est.
Payload to LEO 8,290 kg
Payload to GTO 3,810 kg
Cost
Track record
Launches 3
Successes 1
Failures 2
Success rate 33.3%
Success streak 1
Upcoming launches 0
First flight 1998

Figures from Launch Library 2. Gaps are filled from Wikipedia; “est.” marks a figure that isn't from it (unofficial, or worked out by us: point at it for the basis). A dash means no value for that rocket yet; a cost range counts by its low end; thrust-to-weight and cost per kilogram are worked out from its figures. Launch costs are rough public estimates and can be years old. Cost per kilogram divides the price by the most the rocket can lift to low orbit: that maximum is usually for a version that throws its boosters away, while the price is often for one that lands them, so read it as a best case. Total cost is the fairer comparison. The drawings are to scale but simplified: boosters and fairings follow rounded public figures.

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