Falcon 9 v1.1
From Spacefaring
Q15215794
Falcon 9 v1.1 was the second version of SpaceX's Falcon 9 orbital launch vehicle. The rocket was developed in 2011–2013, made its maiden launch in September 2013, and its final flight in January 2016. The Falcon 9 rocket was fully designed, manufactured, and operated by SpaceX. Following the second Commercial Resupply Services (CRS) launch, the initial version Falcon 9 v1.0 was retired from use and replaced by the v1.1 version.
Wikimedia, Wikidata
payload mass 4850 kilogram, payload mass 13150 kilogram,
Persia, 2013, launch vehicle, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, Reman, United States, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Falcon 9 Stages (1) | Commons | ||
| commons | image | Falcon 9 v1.1 production line | Commons | ||
| commons | image | Falcon 9 and dude on computer | Commons | ||
| commons | image | Falcon 9 first stage test firing (2) | Commons | ||
| commons | image | Falcon 9 Stages (2) | Commons | ||
| commons | image | Falcon 9 1.1 static fire test (9848253816) | Commons | ||
| commons | image | Falcon 9 rollout with TurkmenAlem52E-MonacoSAT to SLC-40 (17108097439) | Commons | ||






