Description: Following second stage separation, SpaceX performed a test flight which attempted to return the first stage of the Falcon 9 through the atmosphere and land it on an approximately 90-by-50-meter (300 ft x 160 ft) floating platform-called the autonomous spaceport drone ship. Many of the test objectives were achieved, including precision control of the rocket's descent to land on the platform at a specific point in the Atlantic ocean, and a large amount of test data was obtained from the first use of grid fin control surfaces used for more precise reentry positioning. The grid fin control system ran out of hydraulic fluid a minute before landing and the landing itself resulted in a crash.
- Information:
- Flight number: 19
- Flight date: 1/10/2015
- Static fire: 12/19/2014
- 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
