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Launch details JCSAT-16

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Description: First attempt to touch down from a ballistic trajectory using a single-engine landing burn. All previous landings from a ballistic trajectory had fired three engines on the landing-burn, which provided more braking force, but subjected the vehicle to greater structural stresses. The single-engine landing burn takes more time and fuel, but puts less stress on the vehicle.

- Information:

  • Flight number: 33
  • Flight date: 8/14/2016
  • Static fire: 8/11/2016
  • Status: Exitoso
Logo del lanzamiento JCSAT-16

Information:

State: Active

Company: SpaceX

First Flight: 2010-06-04

Country: United States

Success Rate: 98%

Description: Falcon 9 is a two-stage rocket designed and manufactured by SpaceX for the reliable and safe transport of satellites and the Dragon spacecraft into orbit.

Details:

- Rocket Details:

  • Height: 70 meters / 229.6 feet
  • Diameter: 3.7 meters / 12 feet
  • Mass: 549054 kg / 1207920 lb
  • Stages: 2
  • Boosters: 0
  • Cost per Launch: $50000000

- Engines:

  • Type: merlin
  • Version: 1D+
  • Layout: octaweb
  • Thrust vacuum:
  • Engine Loss Max: 2
  • Propellant 1: liquid oxygen
  • Propellant 2: RP-1 kerosene
  • Thrust to Weight: 180.1

- Payload Weights:

  • Low Earth Orbit: 22800 kg / 50265 lb
  • Geosynchronous Transfer Orbit: 8300 kg / 18300 lb
  • Mars Orbit: 4020 kg / 8860 lb

- Landing Legs:

  • Number: 4
  • Material: carbon fiber

First and Second Stage

Stage Thrust vacuum kN/lbf Reusable Engines Fuel Amount Tons Burn Time Sec
1 8227 / 1849500 Yes 9 385 tons 162 sec
2 934 / 210000 Yes 1 90 tons 397 sec

- Rocket gallery

Image rocket 1
Image rocket 2
Image rocket 3
Image rocket 4
Image rocket 5
Image rocket 6