Space · launch vehicle

Atlas SLV-3

CONVAIR RETIRED

At a glance

Launches

Success rate

100%

4 ok · 0 failed

Payload to LEO

800 kg

Payload to GTO

—

Manufacturer

Convair

Status

Retired

First flight

01 Jun 1966

Reusable

Height

21 m

Diameter

3.05 m

Launch mass

120 t

Liftoff thrust

3,824 kN

Stages

Launch cost

—

Booster landings

—

Links

Wikipedia

About

The Atlas SLV-3, or SLV-3 Atlas was an American expendable launch system derived from the SM-65 Atlas / SM-65D Atlas missile. It was a member of the Atlas family of rockets.

Source The Space Devs — Launch Library 2 Last checked 29 Sept 2026

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