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Atlas H

Spacecraft and Launch Vehicles

The Atlas H was an American expendable launch system derived from the SM-65 Atlas missile and a member of the Atlas family of rockets that Convair built. It was a stage and a half rocket that used the enhanced Atlas first stage designed for the Atlas G, but without that vehicle's Centaur upper stage, and in practice a separate MSD upper stage flew on all five launches. Atlas H flew only from Space Launch Complex 3E at Vandenberg, where it launched five clusters of NOSS ocean surveillance satellites for the US National Reconnaissance Office; two of those flights also carried LiPS satellites as secondary payloads for the United States Naval Research Laboratory. It could put about 3,630 kg into low Earth orbit or about 2,255 kg into geostationary transfer orbit. The same stage was later reused as the first stage of the Atlas I.

Facts
Year
1983 1
Propulsion
Kerosene 1
Engine Class
Rocket 2
Connections

Derived From

SM-65 Atlas, Vehicles
Source Atlas H (Wikipedia)

Exemplifies

Source Atlas H (Wikipedia)

Of Make

Source SM-65 Atlas (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Encyclopedia Astronautica: Atlas HRelated, Agency
Quote, Related, Agency
Agency Convair

Originated In

Also in Geography Atlas: where this subject originated.

Source Atlas H (Wikipedia)Lead
Quote, Lead
The Atlas H was an American expendable launch system
Sources
1. Encyclopedia Astronautica: Atlas H
Encyclopedia Astronautica
  • Chronology
    5 events 1983 February 9
  • Stage data
    Propellants: Lox/Kerosene.
View the Source
2. Atlas H (Wikipedia)
  • Body
    The Atlas H was a stage and a half rocket
  • Lead
    The Atlas H was an American expendable launch system
View the Source
SM-65 Atlas (Wikipedia)
Lead
Quote, Lead
It was built for the U.S. Air Force by the Convair Division of General Dynamics at an assembly plant located in Kearny Mesa, San Diego.
View the Source
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