- Draco (rocket engine)
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Draco Country of origin United States Manufacturer SpaceX Liquid-fueled engine Propellant nitrogen tetroxide[1] / monomethyl hydrazine[1] Performance Thrust (Vac.) 90 lbf (400 N)[1] Draco is a small hypergolic rocket engine (known as a thruster) designed by SpaceX for use on their Dragon spacecraft[2] and the upper stage of their Falcon 9 rocket.[3]
Contents
Performance and use
Draco thrusters generate 90 pounds-force (400 newtons) of force using a mixture of monomethyl hydrazine fuel and nitrogen tetroxide oxidizer.
Eighteen Draco thrusters will be used on the Dragon spacecraft for attitude control and maneuvering.[1] dual-redundant in all axes: any two can fail and still have complete vehicle control in pitch, yaw, roll and translation.
Four Draco thrusters will be used on the Falcon 9 second-stage as a reaction control system.[3]
See also
References
- ^ a b c d "SpaceX Updates — December 10, 2007". SpaceX. 2007-12-10. http://www.spacex.com/updates_archive.php?page=121007. Retrieved 2010-02-03.
- ^ "SpaceX Draco Thruster Performs Long-Duration Firing and Restart". MarketWatch. December 9, 2008. http://www.marketwatch.com/news/story/SpaceX-Draco-Thruster-Performs-Long/story.aspx?guid=%7B4C11AC71-B20C-4FBA-ADEB-2DB9B8A02B65%7D.
- ^ a b "Falcon 9 Launch Vehicle Payload User’s Guide, 2009". SpaceX. 2009. http://www.spacex.com/Falcon9UsersGuide_2009.pdf. Retrieved 2010=02-03.
External links
- Official SpaceX announcement and test video
- Multiple Draco Test Firings, Test firing video of a set of five Draco thrusters for various intervals, SpaceX, 2010-01-27.
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