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Electric Propulsion for Future Space Missions Part I Bryan Palaszewski Digital Learning Network NASA Glenn Research Center at Lewis Field
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Introduction Why electric propulsion? –Types –Applications Some history Future missions and vehicles A very cool future
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Solar Electric Propulsion Module
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Why High Exhaust Velocity Is Important
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Chemical & Electric Propulsion Have Intrinsic Differences
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Solar and Nuclear Electric Propulsion Subsystems
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Electric Propulsion Historical Overview 1903 -- K. E. Tsiolkovsky derived the “Tsiolkovsky” or “Rocket” Equation commonly used to show the benefits of electric propulsion 1906 -- R. Goddard wrote about the possibility of electric rockets 1911 -- K. E. Tsiolkovsky independently wrote about electric rockets 1929 -- World’s first electric thruster demonstrated by V. P. Glushko at the Gas Dynamics Laboratory in Lenningrad 1960 -- First “broad-beam” ion thruster operated in the U.S. at the NASA Lewis (now Glenn) Research Center
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Electric Propulsion Historical Overview 1964 -- First successful sub-orbital demonstration of an ion engine (SERT I) by the U.S. 1964 -- First use of an electric thruster on an interplanetary probe (Zond 2) by the USSR 1970 -- Long duration test of mercury ion thrusters in space (SERT II) by the U.S. 1972 -- First operation of a xenon stationary plasma thruster (SPT-50) in space (Meteor) by the USSR 1993 -- First use of hydrazine arcjets on a commercial communications satellite (Telstar 401) by the U.S.
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The First Electric Thruster Developed by V. P Glushko at the Gas Dynamics Laboratory in Lenningrad, 1929 - 1933 Solid and Liquid Conductors Were Vaporized by High Current Discharges in the Plenum Chamber and Expanded Through the Nozzle Power Provided by 40 kV, 4 mF Capacitors
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Types Of Electric Thrusters Electrostatic –Ion –Hall Electrothermal –Arcjet –Resistojet Electromagnetic –Magneto plasma dynamic (MPD) –Many others
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Types Of Electric Thrusters
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Ion Thruster
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Ion Thruster Layout
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Hall Thruster SPT-100 1350 W 1600 lb f -s/lb m (Nominal) SPT-70 700 W 1450 lb f -s/lb m (Nominal) SPT-140 4000 W 1700 lb f -s/lb m (Nominal) SPT-50 300 W 1200 lb f -s/lb m (Nominal) Thrusters designed and fabricated by the Design Bureau Fakel, Kaliningrad (Baltic Region), Russia, and offered by International Space Technology, Inc.
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Hall Thruster Magnet Coils Dielectric Walls Cathode Power Supply Xe Anode EzEz BrBr
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Hydrazine Arcjet Primex Aerospace Hydrazine Arcjet: 1.8 kW, 200 mN, 500 lb f -s/lb m
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Arcjet Thruster CATHODE ANODE CURRENT ARC PROPELLANT IN THRUSTER EXHAUST
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Arcjet Thruster Ship Set of Four Olin Aerospace 500 lb f -s/lb m Hydrazine Arcjets and Power Processing Unit
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Magneto Plasma Dynamic (MPD) Thruster Pulsed MPD Thruster Operating on Argon Propellant at Princeton University
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Magneto Plasma Dynamic (MPD) Thruster
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Pulsed Plasma Thruster
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NASA Glenn Electric Propulsion Laboratory (EPL)
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NASA Glenn Electric Propulsion Laboratory (EPL) Contributions On September 23, 2001, the Deep Space 1 ion thruster set a record of 16,000 hrs. of operation while propelling the spacecraft on its encounter with Comet Borrelly. In preparation of MErcury Surface, Space ENvironment, GEochemistry and Ranging (MESSENGER) probe mission, VF-6 was used to characterize components under a 10-sun solar insolation environment. On December 3, 2000, hollow cathodes, which were developed at GRC and tested in VF-5 as part of the Plasma Contactor Unit, began protecting the International Space Station from harmful space plasma voltage potentials.
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NASA Glenn Electric Propulsion Laboratory (EPL) Contributions A refractive secondary concentrator (RSC) achieved temperatures of 1455 Kelvin with an 87% throughput in VF-6. On January 4, 2002, a pulsed plasma thruster on Earth Observing 1 demonstrated a highly fuel efficient method of controlling spacecraft attitude and "pointability." Conducted first integrated solar dynamic system test from solar input to electrical power in VF-6.
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Jupiter
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Saturn
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Uranus
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Neptune
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Neptune and Ion Thruster
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Pluto
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Deep Space 1
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Deep Space 1 Thruster / Spacecraft Compatibility Testing
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Deep Space 1 Thruster
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Launch of Deep Space 1 Boeing Delta II (7326) Rocket October 24, 1998
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DS-1 Trajectory
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Autonomous Navigation
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Comet Borrelly
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