Difference between revisions of "Orbital Sciences Antares"
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Revision as of 10:56, 9 May 2013
The Antares launch vehicle is a two stage rocket with optional third upper-stage, designed and operated by Orbital Sciences Corp. It consists of a kerolox first stage propelled by two Aerojet AJ-26-58 engines and uses a Castor 30 family second stage.
Its launch complex is at the Mid-Atlantic Regional Spaceport (MARS).
Dictionary
- HIF
- Horizontal Integration Facility
- TEL:Transporter-Erecter-Launcher