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OV1-3 - Space launch mission detailed information

MISSION NAME

OV1-3 3

Status

Failure

DATE

28 MAY 1965

LAUNCH PROVIDER

United States Air Force + -img

United States Air Force

Launch Pad

576B3

USA

Description

The OV1 (Orbiting Vehicle 1) were small research satellite to be launched piggy back on Atlas ICBM test flights. They consisted in general of the OV1 satellite and the OV1-PM propulsion module (or upper stage) to reach orbit.

SM-65D Atlas

SM-65D Atlas

USA

Rocket Description

The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage.

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