General Dynamics

Atlas I

I

Retired

Overview

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The Atlas I was a US expendable launch system manufactured by General Dynamics in the 1990s to launch a variety of satellites.

Manufacturer

General Dynamics

Variant

I

Alias

N/A

Maiden Flight

July 25, 1990

Technical Specifications

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43.9 m

Length

3.05 m

Diameter

0 t

Launch Mass

1939 kN

Liftoff Thrust

5900 kg

LEO Capacity

—

GTO Capacity

Launch Record

/03

11

Total Launches

9

Successful

2

Failed

81.8%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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