Article originally published in Aerospace America Magazine
By John Dankanich
It’s been a year of diverse research, innovation and operations in the ﬁeld of electric propulsion.
Japan’s Hayabusa-2 asteroid explorer, propelled by four microwave discharge ion engines, completed its first maneuver in March, setting the stage for the spacecraft to collect a sample from asteroid 1999JU3 and return it to Earth. Also, NASA’s Dawn space-craft achieved orbit around the dwarf planet Ceres. Dawn’s Ion Propulsion System has operated for over 47,000 hours and used 395 kilograms of xenon to deliver approximately 11 kilometers/second of Delta-V, or change in velocity, to the spacecraft.
NASA’s Space Technology 7 demonstration is scheduled for launch in December on the European Space Agency’s LISA Pathfinder Spacecraft to test eight colloid thrusters made by Busek Space and Propulsion Systems of Massachusetts. Also, the Air Force Research Laboratory, the service’s Space and Missile Systems Center and its Rapid Capabilities Ofﬁce collaborated to host a Hall thruster experiment this year aboard the X-37B to characterize performance improvements relative to previous units on board the Advanced Extremely High Frequency spacecraft.
In the area of small-spacecraft propulsion, a micro-cathode arc thruster developed by George Washington University was launched in May. The thruster reduced the initial tumble rates from 30 degrees/second to 1.5 degrees/second within 48 hours of deployment. Also, the Missouri University of Science and Technology is developing a multi-mode system that integrates electrospray with catalytic microtube propulsion.
Iodine technology continues to gain mo-mentum as the iodine Satellite (iSat) project heads toward critical design review at NASA’s Marshall Space Flight Center in Alabama. The spacecraft will demonstrate the BHT-200-I Hall thruster. Also, Busek’s BIT-3 RF ion thruster was selected for flight on the Lunar IceCube Mission.
The PPS 5000 Hall effect thruster from Snecma will be delivered for ﬂight on the Air-bus Eurostar E3000 Electric Orbit Raising (EOR) satellite in 2016 and is scheduled for ﬂight on Eutelsat’s E172B in 2017. Space Systems Loral awarded ﬂight sets of PPS 1350-E Hall thrusters, with 2.5 kilowatt discharge power.
Aerojet Rocketdyne in June announced an agreement to supply its 5 kilowatt XR-5 Hall thruster subsystems for Lockheed Martin’s modernized A2100. A few months earlier, in February, Aerojet Rocketdyne announced agreement to supply XR-5s to Orbital ATK for its all-electric GEOStar 3 satellites. European Space Propulsion is to qualify the XR-5E European variant.
NASA’s Glenn Research Center in Ohio and the Jet Propulsion Laboratory in California continue to develop the 12.5 kilowatt Hall Effect Rocket with magnetic shielding propulsion system. Testing veriﬁed magnetic shielding over 2000-3000 seconds speciﬁc impulse. Integrated thruster Power Processing Unit testing operated at 12.5 kilowatts and up to up to 800 volts.
NASA awarded a cost-share contract to build two NASA Evolutionary Xenon Thruster systems and power processing units as part of a commercial transition project. The hardware has been offered as govern-ment furnished equipment for the latest Discovery Mission opportunity.
NASA Glenn, the Aerospace Corp. and the University of Michigan continued maturation of the annular ion en-gine for high thrust-to-power operation over a broad power and speciﬁc impulse range. Tests of the 65 centimeter thruster demonstrated uniform plasma and broad throttling range with ﬂat car-bon grids.
The University of Stuttgart demonstrated a spherical inertial electrostatic conﬁnement system with anode outlet triggering a jet of both electrons and ions with high kinetic energy with potential high impulse low-power thruster.
At the component level, New Jersey-based Marotta continues to characterize its multi-function valve and completed testing with the Sitael (Alta) 5 kilowatt Hall effect thruster. Also, VACCO Industries of Califor-nia and Alabama delivered custom iodine proportional ﬂow control valves for iSat and completed the qualiﬁcation of proportional ﬂow control module options.
Electrospray work included three Game Changing Development awards to mature 100 micronewton systems to tech-nology readiness level 5 with MIT, JPL and Busek Co. Busek also delivered electronics for its BET-1 (1 millinewton) 100 watt electrospray thruster system.
At high power, NASA NextSTEP pro-pulsion grants were awarded to a team from Aerojet Rocketdyne, University of Michigan and JPL to demonstrate a 100 kilowatt Hall system; to Ad Astra Rocket of Texas for high power, long duration testing of its variable speciﬁc impulse magnetoplasma rocket; and to MSNW of Washington for its electrodeless Lorentz force thruster.