Falcon 9 v1.1

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.

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2013 — 2016  Wikimedia, Wikidata
payload mass 13150 kilogram, payload mass 4850 kilogram, 
Falcon 9, SpaceX, United States, 
Reman, 2010s, Republic of Haiti, 2013, SpaceX CRS-6, SpaceX CRS-4, SpaceX CRS-3, launch vehicle, Dong Fang Hong 2, Tarshish, Sikh Confederacy, SpaceX, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Chinland, Calvinist Republic of Ghent, Ashkenaz, Falcon 9, United States, 

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Location: KML, Cluster Map, Maps,

Frameless

Falcon 9 Stages (1)

Falcon 9 v1.1 production line

Falcon 9 and dude on computer

Falcon 9 first stage test firing (2)

Falcon 9 Stages (2)

Falcon 9 1.1 static fire test (9848253816)

Falcon 9 rollout with TurkmenAlem52E-MonacoSAT to SLC-40 (17108097439)

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