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.

MainWikipediaGalleryBibliographyTableSearch

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

​

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