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DBpedia 2016-04

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Matches in DBpedia 2016-04 for { ?s ?p "Falcon 9 v1.1 is 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.It was designed, manufactured, and operated by SpaceX. Following the second Commercial Resupply Services (CRS) launch, the initial version of the Falcon 9, the v1.0, was retired from use with the v1.1 replacing it. Falcon 9 v1.1 was scheduled to launch crew for NASA under a 2014 contract that enables private organizations to launch crew to the ISS but, in the event, those launches will now be accomplished on a Falcon 9 full thrust version, first flown in December 2015.Falcon 9 v1.1 is a significantly redesigned version of the Falcon 9 v1.0, with 60 percent more thrust and weight. It flew for the first time on a demonstration mission on the sixth overall launch of any Falcon 9 on 29 September 2013.Both stages of the two-stage-to-orbit vehicle use liquid oxygen (LOX) and rocket-grade kerosene (RP-1) propellants. The Falcon 9 v1.1 can lift payloads of 13,150 kilograms (28,990 lb) to low Earth orbit, and 4,850 kilograms (10,690 lb) to geostationary transfer orbit, which places the Falcon 9 design in the medium-lift range of launch systems.The Falcon 9 v1.1 and Dragon capsule combination was used with Falcon 9 v1.1, beginning in April 2014, to resupply the International Space Station under a contract with NASA. SpaceX developed the Falcon 9 v1.1 to be able to carry humans. In late 2014, NASA awarded at least two crewed missions to SpaceX with the Falcon 9 and Crew Dragon, with the potential for up to six.In the event, those missions will fly on the subsequent Falcon 9 version as Falcon 9 v1.1 made its final flight on 17 January 2016."@en }

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