HEMPT-NG Highly Efficient Multistage Plasma Thruster - Next Generation
This project addresses HEMP development activities to three
application fields of electric propulsion systems – LEO, Telecommunication/Navigation and Space
Transportation/Exploration/Interplanetary applications. The HEMP-Thruster concept is an ion propulsion
technology that is based on the use of permanent magnets for plasma confinement. Through this confinement
there is no discharge channel erosion and the technology provides excellent lifetime of the thrusters which is
a unique feature of the HEMP technology. In addition the used cathode technology is backed by several hundred
millions of operational hours of in space operation. Among other advantages, the technology enables very wide
operational ranges and the lowest system complexity of all competing EP technologies creating unique
application possibilities.
The HEMPT-NG proposal addresses the topic COMPET-3-2016-a on
Incremental Technologies which is part of the SRC - In-Space electrical propulsion and station keeping. It
will contribute to the principal target of the EPIC roadmap “to increase the competitiveness of the EP systems
developed in Europe” by developing an integrated solution based on HEMPT for the thruster, the fluidic
management system and the power processing unit. The final project results will consist of two EPS: the first
one ideally suited for LEO applications with a power between 200 to 700 W and the second one optimized for
Telecom/Navigation applications with a power from 3 to 5 kW. Both thrusters will be capable of dual-optimized
mode operations allowing orbit raising and station keeping with the same EPS.
EPIC Workshop 2017 24-25 October 2017 in Madrid – Spain
The EPIC Workshop 2017 was held on 24-25 October 2017 in Madrid – Spain at CDTI
(Centro para el Desarrollo Tecnológico Industrial, Madrid) premises and was organized by EPIC.
TECH COMPARISON ELECTRIC PROPULSION TECHNOLOGIES
The patented European HEMPT-Technology in comparison to the competing
technologies provides unique advantages such as:
- Lowest system complexity due to the simplicity of the concept which will allow
- Maximal reduction of cost and mass,
- Long lifetime by concept,
- Flexibility to provide high thrust operation and very precise low thrust operation with the same engine
- Operation of the same unit in different operating regimes (dual voltage) featuring in orbit selectable ISP maximizing the propellant savings and giving flexibility for new failure recovery strategies.
OUR TEAM The HEMPT-NG consortium
The HEMPT-NG consortium is led by Thales Deutschland GmbH, responsible for
thruster development and integrated EPS. Further European industrial partners are:
POWER PROCESSING UNIT FOR LEO
Belgium
SYSTEM STUDIES / BUSINESS CASES
Germany
SYSTEM STUDIES / BUSINESS CASES
France
POWER PROCESSING UNIT FOR TELECOM./NAV.
Germany
PROJECT COORDINATOR
SYSTEM / THRUSTER MODULE
SYSTEM / THRUSTER MODULE
Germany
Plasmasimulations
Germany
LUIDIC MNGMT. SYSTEM
(FLOW CONTROL UNIT)
(FLOW CONTROL UNIT)
Germany
Testing and analysis
Italy
FLUIDIC MNGMT. SYSTEM
(PRESSURE SUPPLY ASSEMBLY)
(PRESSURE SUPPLY ASSEMBLY)
United Kingdom
PROJECT COORDINATOR
SYSTEM / THRUSTER MODULE
SYSTEM / THRUSTER MODULE
Germany
SYSTEM STUDIES / BUSINESS CASES
Germany
SYSTEM STUDIES / BUSINESS CASES
France
POWER PROCESSING UNIT FOR LEO
Belgium
POWER PROCESSING UNIT FOR TELECOM./NAV.
Germany
Plasmasimulations
Germany
LUIDIC MNGMT. SYSTEM
(FLOW CONTROL UNIT)
(FLOW CONTROL UNIT)
Germany
Testing and analysis
Italy
FLUIDIC MNGMT. SYSTEM
(PRESSURE SUPPLY ASSEMBLY)
(PRESSURE SUPPLY ASSEMBLY)
United Kingdom
An EPS addressing the Telecommunication (GEO) and Navigation (MEO) application
segment with a power range of 3-5 kW, allowing all-electric satellites to save up to 80 % of the propellant
mass (compared to chemical propulsion systems). A LEO EPS addressing the LEO application segment with a power
range 200 W – 700 W, enabling the business cases of the newly emerged LEO constellations e.g. targeting
worldwide internet services access. Assessment of the use of the above-described “GEO” solution for the space
transportation and interplanetary mission application using clustering techniques going up to or beyond 20 kW
of processed spacecraft power, enabling for instance ambitious scientific missions like space travel to Mars
or other planetary rendezvous missions.