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2 NEPTUNE Modular Rockets: Launching the World s Small Sat Payloads!
3 About Founded in 1996 by Roderick and Randa Milliron End-to-end rocket R&D, testing, and manufacturing facilities Two operational rocket engine test sites Location: Mojave Spaceport in California Seeking US Permission to Conduct Orbital Launch Operations (land) at IOS Proposed Private Spaceport, Kingdom of Tonga (pending export control approval) Orbital Launch Operations (ocean): Worldwide. Primary: 160 miles off the California Coast Considering orbital operations from Wallops, Kodiak, and New Mexico (sounding rockets)
4 Project History Pressure-Fed Rocket Engines Since 1995 GPRE 2.5KLMA Liquid Oxygen/Methanol Engine: Thrust = 2,500 lbs. GPRE 0.5KNFA WFNA/Furfuryl Alcohol (Hypergolic): Thrust = 500 lbs. GPRE 0.5KNHXA WFNA/Turpentine (Hypergolic): Thrust = 500 lbs. GPRE 3.0KNFA WFNA/Furfuryl Alcohol (Hypergolic): Thrust = 3,000 lbs. GPRE 6.0KNHXA WFNA/Turpentine (Hypergolic): Thrust = 6,000 lbs. GPRE 10.0KNHXA WFNA/Turpentine (Hypergolic): Thrust = 10,000 lbs. Pressure-Fed Sounding Rockets Since 1999 Neutrino: GPRE 0.5NFA Engine Tachyon: GPRE 3.0KNHXA Engine CPMTV: GPRE 6.0NHXA Engine CPM SR145: GPRE 6.0NHXA Engine Manned Systems Dick Rutan s Global Hilton Project Helium/Hot Air Balloon System Propane Tanks
5 IOS Unique Launch Vehicle Technologies Environmentally Safe, Storable, High-Density Hypergolic Propellants White Fuming Nitric Acid (WFNA) and Turpentine/Furfuryl Alcohol Renewable Fuels derived from Pine Trees and Oat Hulls Instantaneous chemical ignition eliminates need for complex ignition system Low-Cost Propellant Tank Technology Custom aluminum tank liners and tank ends State-of-the-art composite tank reinforcement technology Blowdown Propellant Feed Eliminates the need for turbopumps or a separate pressurant system Unique Rocket Engine Injector Automatically maintains propellant jet flow rate in blowdown mode Maximizes specific impulse over a wide pressure input range Modular Rocket System The Common Propulsion Module (CPM) Low-thrust rocket engines 6,000-10,000lb-thrust engines Smaller engines equal low-cost rocket engine development Small diameter tanks; slosh baffles not required Individual rocket modules can be flight tested at a very low cost Launch vehicle can be customized for any payload by adding modules Designed for assembly-line mass production
6 NEPTUNE Series Modular Rockets The Common Propulsion Module (CPM) is the basic building block of the N-Series Rockets Bi-propellant storable, hypergolic liquid rocket system Blowdown propellant feed State-of-the-art composite propellant tanks Throttleable, ablatively-cooled rocket engines CPMs clustered together in multiples to meet mission requirements
7 IOS Modular Rocket Systems N30 (5 CPMs) Payload = 30 kg 3 stages NanoSat Challenge Olav Zipser High-Altitude Record Jumps N45 (7 CPMs)/ N70(9CPMs) Payload = 45 kg; 70 kg 3 stages NanoSat Challenge N1000 (36 CPMs) Payload = 1,000 kg LEO/ 60kg Lunar Surface 4 stages GLXP/SYNERGY MOON Orbital Tourism Rocket Two-Crew Capsule, 8 orbits
8 N30/N45/N70 Overview Portable, dedicated small sat launchers Easy to transport on highways, ocean, or by air in standard 40-foot cargo container Can be launched from land or sea Launched from land from a Mobile Launch System Launched from the ocean using the Floating Launch or Platform System Storable Propellants/Launch-on-Demand Ultra low-cost, rapid access to space Four Orbital Missions planned for 2012, including NanoSat Challenge Flights
9 CPM Flight Test Program CPM TV: Common Propulsion Module Test Vehicle Low-altitude unguided flight (1) Summer, 2011 (25,000-35,000 ft) FAA Class 3 Waiver Low-altitude guided flights (2) Autumn, 2011 (25,000-50,000 ft) FAA Class 3 Waiver Payloads On-Board: Morehead State University, Kentucky Naval Postgraduate School, California King Abdullah University, Saudi Arabia
10 CPM TV on Mobile Rocket Launcher A full-service mobile rocket launcher Hydraulic lift system Automated propellant-fill hardware Mobile launch platform for IOS CPM SR145 sounding rocket program Suborbital: 145 kg to 310 km
11 IOS TubeSat and CubeSat Kits The $8,000 Orbital Enabler (Special Academic & GLXP Price) PCB Gerber Files 50 Spectrolab TASC solar cells A Li-ion battery pack (3.7 V 5200 mah) Microcomputer (NetMedia BasicX-24) Transceiver (Radiometrix) Antennas Fasteners Complete instructions and assembly guide NEW!!! IOS CUBESAT KIT!!! 1kg Kit and Launch $15,000-$20,000
12 NEPTUNE Launch I Manifest, March 2012: SOLD OUT! CubeSats UC Irvine, UCISAT1 FPT University, Vietnam, F-1 CubeSat Nanyang Technological University, Singapore GLXP Team EuroLuna, Romit 1 (2-Unit CubeSat from Denmark) GLXP Team Plan B (Canada) King Abdullah University, Saudi Arabia (2 IOS CubeSats and 1 TubeSat) TubeSats (constructed from TubeSat Kits): Morehead State University (Kentucky Space) InterAmerican University of Puerto Rico University of Sydney (Australia) (2) i-inspire Project Aslan Academy (Private LA High School) Project Calliope (Space Music Project) Universidad de Puerto Rico / Marcelino Canino Middle School GLXP Team SYNERGY MOON (US/International) GLXP Team Part-Time Scientists / Fluid & Reason Software (2) (US/Germany) Naval Postgraduate School (3) (TubeSats as ad-hoc orbital communication nodes) Defense Science and Technology Lab (DSTL) United Kingdom Austrian Arts Group mur.org United States Military Academy at West Point (2) Brazilian Space Institute /108 5th-7 th Grade Students, Ubatuba, Sao Paulo, Brazil Mexican Satellite Project : ULISES I Arts/Soccer Opera from Space TriVector Services (Huntsville) AKQA Advertising Agency, San Francisco La Despensa (The Pantry) Advertising Agency/Iniciativas en Idiomas (Madrid, Spain) Space Weather.com/ Bishop, CA, High School. ipod = Voyager s Golden Record Twenty additional projects with committed payloads are in various phases of funding. These include academic, arts, private-sector, military, and corporate groups from the US, Mexico, Singapore, Hungary, Japan, Germany, Pakistan, New Zealand, Chile, the Dominican Republic, Holland, France, and Lithuania.
13
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