Orbital Sciences Antares

From OrbiterWiki
Revision as of 08:40, 1 April 2019 by Soumya-8974 (talk | contribs)
Jump to navigation Jump to search

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

See also

w:Antares (rocket)

This article is a stub. You can help Orbiterwiki by expanding it.