Avoiding any liquid and reactive propellants as well as pressurized tanks significantly simplifies handling, integration and launch procedures. Dawn Mk-II Aurora - … Solutions: MicroSpace Nanosatellite micro-propulsion system. 0. View products List your product. 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. Although building blocks are completely self-contained propulsion systems, the whole cluster can be operated as a single plug-and-play unit. The IFM Nano Thruster is a mature technology, developed under ESA contracts for 15 years.

ISIS Deployable Antenna System for 1U/3U CubeSats, ISIS Deployable Antenna System for 6U/12U CubeSats, HEAD Thermister Immersed Infrared Detector, ISIS TXS High Data Rate S-Band Transmitter, ISIS UHF downlink/VHF uplink Full Duplex Transceiver, S-Band Transmitter for Pico and Nanosatellites, ISIS Full Ground Station Kit for VHF/UHF/S-band, S-Band Receiver for HISPICO (Ground Station), ADCS100 – Integrated ADCS with Reaction Sphere, Payload Adapter Systems for Small Satellites, EXA BA0x High Energy Density Battery Array, EXA TITAN-1 High Energy Density Battery Matrix, Cluster of IFM Nano Thruster for Smallsats, EyasSat Single axis air bearing for Attitude Control Studies, ISIS Integration Jig Set for 2U/3U CubeSats, ISIS Integration Jig Set for a 1-Unit CubeSat, ISIS Horizontal Integration Support Jig for 2U/3U, ISIS Vertical Integration Support Jig for 1U/2U/3U, ISIS Stack Integration Jig for a 1-Unit CubeSat Stacks, Kubos Development Service Level Agreement, Kubos Operational Service Level Agreement. The thruster can be operated along the full dynamic range throughout the mission.

Our site uses cookies and other technologies to improve your experience and understand how you and other visitors use our site. The IFM Nano Thruster can operate at an Isp range of 2000 to 6000 s. At any given thrust point, higher Isp operation will increase the total impulse, while it will also increase the power demand. The IFM Nano Thruster contains no moving parts and the propellant is in its solid state at room temperature. Controllable specific impulse up to 6000 S. Due to the efficient ionization process, which allows the capacity 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. SmallSat Propulsion ... Green propulsion that every satellite can use “It is revolutionary to the CubeSat market. The setup has been rigorously lab-tested under vacuum conditions and is certified for use in the space environment. With its IFM Nano Thruster ENPULSION was the first company to offer an operational FEEP-based propulsion solution, which was developed under ESA contracts for 15 years.

Selecting the most appropriate thruster product for a CubeSat can be a tricky challenge.

from 40,000.00. ISIS Deployable Antenna System for 1U/3U CubeSats, ISIS Deployable Antenna System for 6U/12U CubeSats, HEAD Thermister Immersed Infrared Detector, ISIS TXS High Data Rate S-Band Transmitter, ISIS UHF downlink/VHF uplink Full Duplex Transceiver, S-Band Transmitter for Pico and Nanosatellites, ISIS Full Ground Station Kit for VHF/UHF/S-band, S-Band Receiver for HISPICO (Ground Station), ADCS100 – Integrated ADCS with Reaction Sphere, Payload Adapter Systems for Small Satellites, EXA BA0x High Energy Density Battery Array, EXA TITAN-1 High Energy Density Battery Matrix, Cluster of IFM Nano Thruster for Smallsats, EyasSat Single axis air bearing for Attitude Control Studies, ISIS Integration Jig Set for 2U/3U CubeSats, ISIS Integration Jig Set for a 1-Unit CubeSat, ISIS Horizontal Integration Support Jig for 2U/3U, ISIS Vertical Integration Support Jig for 1U/2U/3U, ISIS Stack Integration Jig for a 1-Unit CubeSat Stacks, Kubos Development Service Level Agreement, Kubos Operational Service Level Agreement, 1 axis 1/3U CubeSat Cold-Gas micropropulsion system, 2 axis 1/3U CubeSat Cold-Gas micropropulsion system, 1 axis full 1U CubeSat Cold-Gas micropropulsion system, 2 axis full 1U CubeSat Cold-Gas micropropulsion system. ... Price on request Home / Propulsion & pressurisation.

This is achieved by the use of two cold-redundant electron sources acting as neutralizers. As of April 2020, there are 28 IFM Nano Thrusters on 9 spacecrafts in orbit with total deliveries exceeding 100 thrusters. The setup has been rigorously lab-tested under vacuum conditions and is certified for use in the space environment. It offers 3-axis stabilization, based on proven, reliable MEMS technology.

The system is modular and customizable and is already integrated on a number of CubeSats that are ready for flight. With a 1,000x higher thrust than electric-based systems, operators can get online faster, stay online longer and ensure their responsible operations. 20.00. Once electrons have left the neutralizer, they will be pulled towards the positive potential of the ion plume. €50000 - €210000.

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Mission Deliver Position Return Products. Media ... CubeSat Propulsion Module. As the IFM Nano Thruster expels an ion current of up to 4 mA, the module needs means to prevent spacecraft charging. Electrothermal systems remain a promising technology for CubeSat propulsion because it can operate with inert propellants, does not require the CubeSat to carry combustible material, and can be used with storable propellants.

Rapid growth of the NewSpace sector has led to greater use of modular components, like thrusters.

Mature technology. It offers 3-axis stabilization, based on proven, reliable MEMS technology. 0. The IFM Nano Thruster can be clustered in order to meet any specific mission need. The PPU is able to measure and control this charge balancing electron current. SmallSat Propulsion. In this article, we look at some of the factors that should be taken into account to make this decision. Antenna systems. Swag Shop. Media Careers 0. Showing all 3 results Cluster of IFM Nano Thruster for Smallsats. CubeSat Propulsion. from 42,000.00. This MicroSpace MEMS-based Micropropulsion System is suitable for CubeSats of 1 kg up to small microsatellites up to 100kg.

Safe and inert system compliant during launch.

The thrust can be controlled through the electrode voltages, providing excellent controllability over the full thrust range and a low thrust noise. SmallSat Propulsion Thruster - 20N.
ISIS Deployable Antenna System for 1U/3U CubeSats, ISIS Deployable Antenna System for 6U/12U CubeSats, HEAD Thermister Immersed Infrared Detector, ISIS TXS High Data Rate S-Band Transmitter, ISIS UHF downlink/VHF uplink Full Duplex Transceiver, S-Band Transmitter for Pico and Nanosatellites, ISIS Full Ground Station Kit for VHF/UHF/S-band, S-Band Receiver for HISPICO (Ground Station), ADCS100 – Integrated ADCS with Reaction Sphere, Payload Adapter Systems for Small Satellites, EXA BA0x High Energy Density Battery Array, EXA TITAN-1 High Energy Density Battery Matrix, Cluster of IFM Nano Thruster for Smallsats, EyasSat Single axis air bearing for Attitude Control Studies, ISIS Integration Jig Set for 2U/3U CubeSats, ISIS Integration Jig Set for a 1-Unit CubeSat, ISIS Horizontal Integration Support Jig for 2U/3U, ISIS Vertical Integration Support Jig for 1U/2U/3U, ISIS Stack Integration Jig for a 1-Unit CubeSat Stacks, Kubos Development Service Level Agreement, Kubos Operational Service Level Agreement. CubeSat Propulsion.

Products. Our site uses cookies and other technologies to improve your experience and understand how you and other visitors use our site. Propulsion and pressurissation systems for CubeSats and nanosats.

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