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Launch details ABS-2A / Eutelsat 117W B
No description provided
Description:
One year after pioneering this technique on flight 16, Falcon again launched two Boeing 702SP gridded ion thruster satellites in a dual-stack configuration, with the two customers sharing the rocket and mission costs. First stage landing attempt on drone ship failed on landing due to low thrust on one of the three landing engines.
- Information:
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Flight number: 31
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Flight date: 6/15/2016
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Static fire: 6/13/2016
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Status: Exitoso
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:
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Height: 70 meters / 229.6 feet
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Diameter: 3.7 meters / 12 feet
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Mass: 549054 kg / 1207920 lb
- Stages: 2
- Boosters: 0
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Cost per Launch: $50000000
- Engines:
- Type: merlin
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Version: 1D+
- Layout: octaweb
- Thrust vacuum:
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Engine Loss Max: 2
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Propellant 1: liquid oxygen
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Propellant 2: RP-1 kerosene
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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
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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 |
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