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Falcon 9

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Falcon 9
NameFalcon 9
CaptionA Falcon 9 Block 5 at Launch Complex 39A
FunctionOrbital launch vehicle
ManufacturerSpaceX
Country originUnited States
Height70, m, ft
Diameter3.66, m, ft
Mass549, t, lb
Capacity LEO22.8, t, lb
Capacity GTO8.3, t, lb
StatusActive
Launches350+ (as of May 2024)
Success348
Failures2 (Amos-6 & CRS-7)
First4 June 2010
LastActive
SitesCCSFS, KSC, VSFB

Falcon 9 is a partially reusable, two-stage medium-lift launch vehicle designed and manufactured by the American aerospace company SpaceX. It is powered by nine Merlin engines on its first stage and a single Merlin Vacuum engine on its second stage, enabling it to deliver payloads to a wide range of orbits, including low Earth orbit (LEO) and geostationary transfer orbit (GTO). The rocket is renowned for its pioneering reusability, with its first stage capable of landing vertically after launch to be refurbished and flown again, a technology that has dramatically reduced the cost of access to space. Since its debut in 2010, it has become one of the world's most frequently launched orbital rockets, serving commercial, civil, and national security customers.

Overview

The vehicle was developed under the leadership of Elon Musk to provide reliable and cost-effective launch services, fundamentally challenging the economics of the global launch industry. Its operational profile includes missions for NASA, such as Commercial Resupply Services (CRS) flights to the International Space Station and the Commercial Crew Program's Crew Dragon spacecraft, as well as deploying large constellations like Starlink for SpaceX. The rocket's first-stage booster landings are often conducted on autonomous spaceport drone ships, such as *Just Read the Instructions* and *A Shortfall of Gravitas*, in the Atlantic Ocean or Pacific Ocean.

Design and development

Initial design work began in the mid-2000s, with the first version, Falcon 9 v1.0, flying from SLC-40. The design evolved through several major iterations: v1.1 introduced an Octaweb engine arrangement and lengthened tanks, while the Full Thrust (v1.2) variant featured subcooled propellants for increased performance. The current and final operational version, Block 5, debuted in 2018 with upgrades focused on reusability and reliability, including improved Merlin 1D+ engines, a thermal protection system, and retractable landing legs. Key to its reusability is the first stage's ability to perform controlled re-entry burns and precise propulsive landings, guided by cold gas thrusters and grid fins.

Operational history

The inaugural flight on June 4, 2010, successfully carried a boilerplate Dragon capsule. Early milestones included the first commercial mission to the International Space Station in 2012 under the NASA Commercial Orbital Transportation Services program. The program suffered two in-flight failures: the CRS-7 mission in 2015 due to a strut failure in the second stage, and the Amos-6 anomaly in 2016 during a pre-launch static fire test. A cornerstone achievement was the first successful booster landing in December 2015 at Landing Zone 1, followed by the first drone ship landing on the *Of Course I Still Love You*. The rocket has since launched astronauts for NASA from LC-39A and completed hundreds of missions, including a record-setting number of launches in a single year.

Variants and derivatives

The primary evolution includes the retired Falcon 9 v1.0, v1.1, and the Full Thrust configurations leading to the operational Block 5. A heavier-lift derivative, the Falcon Heavy, consists of a strengthened core stage flanked by two additional Falcon 9 first stages acting as side boosters. While the Falcon 1 was an earlier, smaller vehicle, the Starship and Super Heavy represent SpaceX's next-generation, fully reusable system intended to eventually supersede it for the most demanding missions. Specialized missions have also used flight-proven boosters, designated with a "B" serial number, demonstrating extensive reuse.

Specifications

The Falcon 9 Block 5 stands approximately 70 meters tall with a diameter of 3.66 meters. The first stage is powered by nine Merlin 1D+ engines burning RP-1 and liquid oxygen, producing over 7.6 meganewtons of thrust at sea level. The second stage uses a single Merlin Vacuum engine optimized for operation in space. It can deliver up to 22.8 metric tons to low Earth orbit and up to 8.3 metric tons to geostationary transfer orbit, performance that varies based on the mission profile and booster recovery mode. The payload fairing is 13.1 meters tall and can be optionally recovered.