Transcription of SpaceX Propulsion
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SpaceX Propulsion Tom Markusic Space Exploration Technologies 46th AIAA/ASME/SAE/ASEE. Joint Propulsion Conference July 28, 2010. Friday, August 6, 2010. SpaceX Propulsion Tom Markusic Space Exploration Technologies 46th AIAA/ASME/SAE/ASEE. Joint Propulsion Conference July 28, 2010. Friday, August 6, 2010. Overview Inverse Hyperbolic Bessel Functions Friday, August 6, 2010. Near-term Propulsion Needs Friday, August 6, 2010. Near-term Propulsion Needs HLLV Propulsion Merlin 2 uses scaled-up, flight proven Merlin 1 design J-2X SpaceX can develop and flight qualify the Merlin 2 engine in ~3. years at a cost of ~$1B. Production: ~$50M/engine J-2X development already in progress under Constellation Merlin 2 J-2X. program Propellant LOX/RP LOX/LH2. Merlin 2 Thrust (vac) [klbf] 1,700 292. Isp (vac) [sec] 322 448. T/W [lbf/lbm] 150 55. Friday, August 6, 2010. Near-term Propulsion Needs HLLV Propulsion Solar Electric Propulsion for Cargo Tug Merlin 2 uses scaled-up, flight Cluster of ~5 high TRL thrusters proven Merlin 1 design NEXT process 100 kWe solar power J-2X SpaceX can develop and flight Ion Thruster Next generation tug uses single qualify the Merlin 2 engine in ~3 high power thruster, such as NASA.
SpaceX Propulsion Tom Markusic Space Exploration Technologies 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference July 28, 2010 Friday, August 6, 2010
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