Antares 1A

retired American solid propellant rocket stage

MainGalleryBibliographyTableSearch

1960 — 1970  Wikidata
specific impulse by weight 256 second, mass 1225 kilogram, diameter 0.78 metre, height 3.38 metre, maximum thrust 60.5 kilonewton, 
rocket stage, solid-propellant rocket, United States, 
United States, Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, 1960, Republic of Haiti, 1960s, 

​

Location: KML, Cluster Map, Maps,

Type	Subtype	Date	Description	Notes	Source