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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.
Falcon 9 is a partially reusable, human-rated, two-stage-to-orbit, medium-lift launch vehicle [a] designed and manufactured in the United States by SpaceX.The first Falcon 9 launch was on 4 June 2010, and the first commercial resupply mission to the International Space Station (ISS) launched on 8 October 2012. [14]
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Falcon 9 B1060 was a Falcon 9 first-stage booster manufactured and operated by SpaceX. It was the senior active booster vehicle for the company [1] since the demise of B1058 on 25 December 2023 during transit back to shore, until being expended for the Galileo FOC FM25 & FM27 mission on 28 April 2024. [2] It had flown 20 missions and landed 19 ...
English: From left to right: Falcon 1 with payload fairing; Falcon 9 version 1.0 with Dragon 1 (cargo) spacecraft; Falcon 9 version 1.1 Reusable with Dragon 1 (cargo) spacecraft
Rockets from the Falcon 9 family have a success rate of 99.32% and have been launched 441 times over 15 years, resulting in 438 full successes, two in-flight failures (SpaceX CRS-7 and Starlink Group 9–3), one pre-flight failure (AMOS-6 while being prepared for an on-pad static fire test), and one partial failure (SpaceX CRS-1, which delivered its cargo to the International Space Station ...
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 ...
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).