Head to head

Atlas IIAS vs Zenit-2

Two vehicles in the same payload class. Every figure below comes from the same two sources for both rockets, and a row appears only when both publish the input.

Payload to low Earth orbit

Relative

Atlas IIAS: 6,580 kg

Zenit-2: 13,740 kg

Side by side

8 comparable figures

The highlighted value wins the row. Rows where neither direction is better, like length or stage count, highlight nothing.

Metric	Atlas IIAS	Zenit-2
Flights flown	30	35
Success rate	100%	82.9%
Payload to LEO (kg)	6,580	13,740
Liftoff thrust (kN)	4,391	7,300
Length (m)	47.54	57
Diameter (m)	3.04	3.9
Launch mass (t)	204	459
Stages	3	2

Atlas IIAS

Flight record

100% success rate30 of 30 flown

1993peak 1997 · 5 flights2004

Maiden flight 1993-12-16. Retired.

Zenit-2

Flight record

82.9% success rate29 of 35 flown · 6 failed

1985peak 1987 · 5 flights2004

Maiden flight 1985-04-13. Retired.

Atlas IIAS is built by Lockheed Martin of the United States (company profile on Space Index).Zenit-2 is built by Yuzhnoye Design Bureau of Ukraine.

Full specifications and the complete launch history for each: Atlas IIAS · Zenit-2.

Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.