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astronautix.com Atlas H


Family: Atlas. Country: USA. Status: Hardware.

Atlas H used the Atlas first stage developed for the Atlas G vehicle. It was flown without the Centaur upper stage.


Specifications

Launches: 5. Failures: 0. Success Rate: 100.00% pct. First Launch Date: 08 February 1983. Last Launch Date: 15 May 1987. LEO Payload: 3,630 kg. to: 185 km Orbit. Payload: 2,255 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 197,750 kgf. Total Mass: 150,540 kg. Core Diameter: 3.1 m. Total Length: 27.0 m. Launch Price $: 50.00 million. in 1994 price dollars. Flyaway Unit Cost $: 50.00 million. in 1985 unit dollars.


Atlas H Chronology


1983 Feb 8 - - 13:47 GMT. LV Configuration: Atlas s/n 69F / 6001H. Launch Site: Vandenberg . Launch Complex: SLC3E.
1983 Jun 9 - - 23:23 GMT. LV Configuration: Atlas s/n 69F / 6002H. Launch Site: Vandenberg . Launch Complex: SLC3E.
1984 Feb 5 - - 18:44 GMT. LV Configuration: Atlas s/n 69F / 6003H. Launch Site: Vandenberg . Launch Complex: SLC3E.
1986 Feb 9 - - 10:06 GMT. LV Configuration: Atlas s/n 69F / 6004H. Launch Site: Vandenberg . Launch Complex: SLC3E.
1987 May 15 - - 15:45 GMT. LV Configuration: Atlas s/n 69F / 6005H. Launch Site: Vandenberg . Launch Complex: SLC3E.

Bibliography:



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Last update 12 March 2001.
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