Description: Total payload mass was 1,316 kg (2,901 lb) : 6 satellites weighing 172 kg each, plus two 142-kg mass simulators. This was the second Falcon 9 booster equipped with landing legs. Following second-stage separation, SpaceX conducted a controlled-descent test of the first stage, which successfully decelerated from hypersonic velocity in the upper atmosphere, made reentry and landing burns, deployed its legs and touched down on the ocean surface. As with the previous mission, the first stage then tipped over as expected and was not recovered.
- Information:
- Flight number: 15
- Flight date: 7/14/2014
- Static fire: 12/19/2015
- Status: Exitoso
- Bibliography:
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
