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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. Falcon 9 v1.1 was a significant evolution from Falcon 9 v1.0, with 60 percent more thrust and weight.
Left to right: Falcon 9 v1.0, v1.1, v1.2 "Full Thrust", Falcon 9 Block 5, Falcon Heavy, and Falcon Heavy Block 5. A Falcon 9 first-stage booster is a reusable rocket booster used on the Falcon 9 and Falcon Heavy orbital launch vehicles manufactured by SpaceX.
The first version of the Falcon 9, Falcon 9 v1.0, was developed in 2005–2010, and flew five orbital missions in 2010–2013. The second version of the launch system—Falcon 9 v1.1—has been retired meanwhile. Falcon 9 v1.1 was developed in 2010–2013, and made its maiden flight in September 2013.
The third version of the Falcon 9 was developed in 2014–2015 and made its maiden flight in December 2015. The Falcon 9 Full Thrust is a modified reusable variant of the Falcon 9 family with capabilities that exceed the Falcon 9 v1.1, including the ability to "land the first stage for geostationary transfer orbit (GTO) missions on the drone ship" [14] [15] The rocket was designed using ...
Falcon 9 v1.0 (left) and v1.1 (right) engine configurations The launch of the first Falcon 9 v1.1 from Vandenberg SLC-4 (Falcon 9 Flight 6) in September 2013. V1.1 is 60% heavier with 60% more thrust than v1.0. [74] Its nine (more powerful) Merlin 1D engines were rearranged into an "octagonal" pattern [89] [90] that SpaceX called Octaweb. This ...
Falcon Heavy is a heavy-lift derivative of Falcon 9, combining a strengthened central core with two Falcon 9 first stages as side boosters. [1] Falcon 9 at Dish Network's Littleton, Colorado office. The Falcon design features reusable first-stage boosters, which land either on a ground pad near the launch site or on a drone ship at sea. [2] In ...
The Falcon 9 v1.0 first stage was used on the first five Falcon 9 launches, and powered by nine SpaceX Merlin 1C rocket engines arranged in a 3x3 pattern. Each of these engines had a sea-level thrust of 556 kN (125,000 pounds-force) for a total thrust on liftoff of about 5,000 kN (1,100,000 pounds-force).
The sixth flight of the Falcon 9 launch vehicle launched in September 2013, which was the maiden flight of Falcon 9 v1.1. [2] The site was used for a second time in January 2016 for the Jason-3 launch (which was the last flight of Falcon 9 v1.1) and for a third time in January 2017 for the first of the Iridium Next launches.