For 15 years, FOTEC has followed a technology push from ESA developing a FEEP propulsion technology for a precise orbit control of scientific satellites in formation flight. The adaptation of an established FEEP (field emission electric propulsion) ion thruster design for use on micro and nano satellites (particularly CubeSats). Summary Enpulsion's IFM Nano thruster has been developed and extensively tested in cooperation with the European Space Agency.

A spin-off company was founded (Enpulsion GmbH) that commercially sells the thruster. Mechanically, the thruster comprises a tank filled with the metal propellant and rigidly connected to the crown emitter. Our company delivers innovative products of superb quality to great customers. Both engineering models are subjected to environmental tests including shock and vibration tests, thermal vacuum tests and performance tests. Also the lifetime as well as lifetime limiting factors are currently not known. Then please fill in this form and we will get back to you with more details. ENPULSION is Driving Your Advance – Feel free to contact us! Requests that are submitted through satsearch are anonymously posted to our leads page. Electrically, the thruster is commanded via the spacecraft bus via I2C or UART. The IFM Nano Thruster is a mature technology, developed under ESA contracts for 15 years. satsearch.co is participating in the ESA Business Incubation Centre Noordwijk. In the present design, only COTS components are used for thermal sensors and electronics. Due to the efficient ionization process which allows one to ionize up to 60% of the evaporated Indium atoms, the IFM Nano Thruster can provide a higher specific impulse than any other ion propulsion system currently on the market. +1 (408) 599-3030 Phone USA Office: While the required power to operate the IFM Nano Thruster starts at around 8 W, at higher thrust levels one can choose between high thrust and high specific impulse operation. The IFM Nano Thruster can operate at an isp range of 2,000 to 6,000 seconds. Join them! Since 2015, the number of CubeSats launched has increased over 250%. Would you like to receive additional information? Please report any mistakes to us. The primary objectives for project IFM Nano are: The IFM Nano Thruster addresses the urgent need of a propulsion system for micro- and nano-satellites: its wide range of thrust (1μN to 1mN), the excellent throttlability, and a high specific impulse (up to 5000 s), allow to significantly increase the mission range of such satellites in low orbits. Join them! © satsearch.co, 2015 - 2020 All Rights Reserved. The IFM Nano Thruster can operate at an isp range of 2,000 to 6,000 seconds. The IFM Nano thruster has been developed and extensively tested in cooperation with the European Space Agency. The IFM Nano thruster module is used as a compact pre-qualified building block in order to provide custom solutions at a commodity price and ultra-short lead times. Controllable specific impulse up to 5,000 seconds, I accept the General Sales Conditions and consent. Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. The thruster shall be able to operate, however, for at least a couple of years in a radiation environment typically expected in LEO.

Any plume divergence shall be minimised as much as possible. ALL RIGHTS RESERVED, European Data Relay Satellite System (EDRS), SAT-AIS - Satellite Automatic Identification System, 4S - Space Systems for Safety and Security. At present, the shape if the plume as well as its characteristics are unknown. All the work as outlined in the project plan is performed. The PPU is able to measure and control this charge balancing electron current. The IFM Nano Thruster is a mature technology, developed under ESA contracts for 15 years. If you continue to use this site we will assume that you are happy with it.

Monolithic outer structure in a 10x10x10 cm³ package weighting less than 1 kg, including electronics, tank, and thruster. Three dedicated test campaigns are initiated: The project is finished.

All rights reserved. Phone EU Office: In this time more than 100 emitter have been tested and an ongoing lifetime test has demonstrated more than 20,000 h of firing without degradation of the emitter performance.

First thrusters have been successfully demonstrated in orbit in January 2018! 2700 Wiener Neustadt, Austria, One Boston Place, Suite 2600 +43 2622 4170121 a plume diagnostics system is designed and used to characterise the plume of the IFM Nano Thruster. Enpulsion's IFM Nano thruster has been developed and extensively tested in cooperation with the European Space Agency. The IFM Nano Thruster provides a nominal thrust of 350 µN and can operate at an Isp range of 2,000 to 6,000 s. It can be operated along the full dynamic range throughout the mission. *I hereby accept to receive further information. The high Isp on the other hand allows for very high delta-v manoeuvres at a high propellant mass utilization efficiency (80%).

This means that high isp and low isp maneuvers can be included in a mission planning, as well as high thrust orbit maneuver and low thrust precision control maneuvers. Availability: 16 weeks ENPULSION has been founded as a Spin-Out together with FOTEC to meet this market demand by preparing to scale the production of this thruster to several hundred units per year. Several thruster are currently flying in space. An optional housing encloses all parts but is not required for mechanical stability. Enpulsion's IFM Nano thruster has been developed and extensively tested in cooperation with the European Space Agency. A full characterization and test campaign including functional and environmental tests to verify the design’s specifications and its fitness to operate reliably in orbit. The extractor anode, which is part of the top plate, is separated via an isolator from the electronics compartment and the tank.

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COPYRIGHT 2020 © EUROPEAN SPACE AGENCY. I accept the General Sales Conditions and consentI accept the General Sales Conditions and consent. As interest in space continues to expand, so does the number of new space companies founded each year.

More than 100 emitters have been tested and an ongoing lifetime test has demonstrated more than 18.000 hours of firing without degradation of the emitter performance. Email: contact form. The IFM Nano Thruster shall be able to survive typical loads expected during ground handling and LEOP. Worlds First Commercial Spherical Reaction Wheel. Power interfaces 3.3V and 12V, control via I2C or UART, No moving parts, all-solid in OFF state (during launch), Fully tested according to relevant ESCC standards, COTS components tested for radiation and thermal compliance, a test campaign for cathodes is performed to investigate failure mechanism as well as to select the most suitable cathode for our application, the PPU subjected to low dose as well as high dose radiation tests to determine how much radiation the PPU equipped with COTS components can survive and to identify components most vulnerable to radiation. The central command and control module is connected to the independent power supplies for the heater, the two cathodes (two separate supplies), the emitter, and the extractor. FOTEC Forschungs- und Technologietransfer GmbH. Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. The combination of high Isp with medium very well controllable thrust levels in a small and light package makes the IFM Nano thruster a strong competitor for existing colloid, cold gas, or Hall effect thrusters.

AMR propulsion aims to solve these problem with a unique, modular product: the IFM Micro Thruster, a compact, modular propulsion system suitable for all small satellites ranging 1-500 kg, with the highest propellant efficiency, capable of controlling satellites’ position with an unprecedented accuracy, perfectly suitable for single CubeSats as well as for big constellations of satellites (>100).

CONTROLLABLE SPECIFIC IMPULSE UP … As of April 2020, there are 28 IFM Nano Thrusters on 9 spacecrafts in orbit with total deliveries exceeding 100 thrusters.

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First Thrusters had been successfully demonstrated in orbit in January 2018! The IFM Nano Thruster is a miniaturised ion thruster – with an electric field applied to accelerate electrically-charged atoms (known as ions) to produce thrust – based around a porous tungsten crown, seen at the centre of the thruster, which is used to emit liquid metal indium ions. The plasma plume shape partly determines the thruster efficiency. The thruster can be operated along the full dynamic range throughout the mission.

201 Washington Street This very mature and worldwide unique technology is meeting a strong need in an emerging market of satellite constellations (hundreds of small satellites performing a task together). The IFM Thruster family is a mature technology, developed under ESA contracts for 15 years. delivers innovative products of superb quality to great customers.

This is achieved by the use of two cold-redundant electron sources acting as neutralizers. The IFM Nano Thruster addresses the urgent need of a propulsion system for micro- and nano-satellites: its wide range of thrust (1μN to 1mN), the excellent throttlability, and a high specific impulse (up to 5000 s), allow to significantly increase the mission range of such satellites in low orbits. The functionality of the neutralization concept is based on extensive simulation of the electric fields, but no experimental verification has been conducted so far.

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