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Published byNoah Daniel Reed Modified over 9 years ago
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ERPS Presentation Space Access 2000 Scottsdale, AZ April 27th - 29th, 2000
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The Five W’s Who Self-funded Volunteer Non-Profit 501(c)(3) What Liquid Fuel Rocket Engine Development Where San Jose, CA (“Silicon Valley”) When Founded - Feb 1993 Why “It seemed like a good idea at the time”
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Staged Development Catalyst Development –Old Technology –New Technology Engine Tests –Basic Performance –Catalyst Optimization –Size Scalability –Multi Engine Capabilities –Bi Propellant Capabilities –Flight Weight Verification Tests
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Flight Vehicles POGO –Engine & Flight Controls test vehicle –DC-X “Conrad Square” flight plan ReSOAR –Reusable Sub-Orbital Atmospheric Research –Aerospike engine tests –Exo-atmospheric / Re-entry / Restart tests PROTO –Private Rocket to Orbit Tiny Objects –SSTO “proof of concept” vehicle
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Commercial Vehicles Alpha Class –Reusable SSTO demonstration –3000 lbs to LEO –5000 lbs Point to Point –1 hour to anywhere –Automated flight operations –Fast package transport market –“Executive Jet” market
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Commercial Vehicles Bravo Class –Reusable, Refuelable SSTO transport –15,000 lbs to LEO –25,000 lbs Point to Point –70 passenger “spaceliner” – 5 + 1 = 15K to “Clarke” GEO orbit –10 + 1 = 15K to surface of moon Return empty –15 + 1 = 15K to surface of moon 15k lunar return
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Recent Events Static engine firings Vehicle mockup Software development Beowulf cluster Site hunt FAA input For-Profit spinoffs Funding issues
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How To Get Involved Web page - www.erps.org Email list Contributions of: –Material –Code –Computing cycles –Money Think, dream, talk and do!
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