Falcon 9 v1.1

retired

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Specifications

Status: retired
Height: 68.4 m
Diameter: 3.65 m
Mass: 506,000 kg
Stages: 2
Thrust: 5,883 kN
Payload to LEO: 13,150 kg
Payload to GTO: 4,850 kg
First flight: 2013-09-29
Total launches: 15
Success / Fail: 14 / 1

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.

Propulsion

First stage

9×Merlin 1D845 kN

RP-1 / LOX · gas-generator

SpaceXIsp 311s (vac)since 2013

Second stage

Merlin 1D Vacuum981 kN

RP-1 / LOX · gas-generator

SpaceXIsp 348s (vac)since 2013

Specifications

Propulsion

First stage

Second stage

Payloads it launched