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For science and exploration players, who require access to space operations and data services, SAVOMID offers fastest in-space service at a fraction of the low cost and complexity. You can test your payload in space.

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Products

Structure SAV-MCS110

The SAVOmid CubeSat structures as generic structure is appropriate for any type of standard cubesats.

These structures can be ordered in size of 1U, 2U, 3U, 6U, 12U, 16U that permit CubeSat developers maximum flexibility in their design process. In addition, adding detachable shear panels are available.

These structures are suitable for any type of PCBs and other flight modules.

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POD SAV-LPO110

The SAVOmid CubeSat POD is a launch adapter that provides simple, well-defined interfaces between the CubeSat and the launch vehicle.

CubeSats are fully enclosed into the POD and they launch with the signal of the launch vehicle. These are non-explosive devices which are testable and reusable.

These structures can be ordered in size of 1U, 2U, 3U, 6U, 12U, 16U.

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Air-bearing SAV-IAB110

Air bearing is a functional test infrastructure for satellite Attitude Determination and Control Subsystems (ADCS). Its working procedure and frictionless movement simulates the zero-g condition which Satellite experience in the orbit. By using this, satellite is capable to rotate around 3 axis roll, pitch and yaw.

Air bearing is necessary to evaluate the ADCS Algorithms and Softwares. Also, the performance of Actuators and sensors of the satellite can be tested in real situation to minimize the risk of error.

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Sun Sensor SAV-SSS110

The Sun Sensor SAV-SSS110 determines the spacecraft body angles with respect to the sun. The sensor has two axis and provides low-cost, high-accuracy and low power consumption concurrent to be the perfect ADCS solution for nanosatellite platforms like CubeSats.

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Battery Monitoring Unit SAV-EBM110

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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Power Control Unit SAV-EPC110

Power Control Unit manages charging the batteries using the power that is generated by solar cells. In order to do this, power point tracking Converters are utilized. This unit privides 5 regulated power lines with high efficient DC/DC converter. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure condition. It is highly adaptable for different subsystems in small LEO satellites.

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 OBC Board SAV-EOB110

This On Board Computer, based on Hercules microcontroller with integrated safety features, is designed as the central processor for high reliable space applications. The module is resistant to radiation effects and guarantees 3 years reliable operation in LEO missions. All environmental tests are subjected to ECSS-10-03 standard.

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OBC Board SAV-EAO111

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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Reaction wheel SAV-ARW110

SAVomid reaction wheel is installed on the satellite and by combining the speed of reaction wheels, the satellite can be rotated around three axes or a combination of these three axes. Commands for each of the wheels installed on the satellite are sent by the command center to the satellite receiver and applied to the wheels via the internal network. The reaction wheel actuator is mainly used to control the status of the satellite. These actuators are able to provide the torque and momentum required to maneuver and stabilize the satellite.

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Reaction wheel SAV-ARW111

SAVomid reaction wheel by combining the speed of reaction wheels, the satellite can be rotated around three axes or a combination of these three axes. Commands for each of the wheels installed on the satellite are sent by the command center to the satellite receiver and applied to the wheels via the internal network. The reaction wheel actuator is mainly used to control the status of the satellite. These actuators are able to provide the torque and momentum required to maneuver and stabilize the satellite.

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Reaction wheel SAV-ARW112

The SAVomid CubeWheel Small by combining the speed of reaction wheels, the satellite can be rotated around three axes or a combination of these three axes. Commands for each of the wheels installed on the satellite are sent by the command center to the satellite receiver and applied to the wheels via the internal network. SAVomid CubeWheel Small is mainly used to control the status of the satellite. These actuators are able to provide the torque and momentum required to maneuver and stabilize the satellite.

The SAVomid CubeWheel Small is a miniature reaction/momentum wheel used to control the attitude of a CubeSat.

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Magnetorquer SAV-AMT110

Magnetorquer is one of the practical actuators which generates magnetic Torques and changes the total momentum of the satellite. Its used to control the attitude of satellite beside other actuators like reaction wheel or thruster.

The type of alloys used to make these actuators is very crucial. In other words, the high magnetic permeability coefficient of the nucleus and the low magnetic residue in the nucleus are very important.

The linearity of the magnetic field generated by this actuator as well as the current and time characteristics when the core is saturated are very important parameters in this actuator.

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Magnetorquer SAV-AMT111

Magnetorquer is one of the practical actuators which generates magnetic Torques and changes the total momentum of the satellite. Its used to control the attitude of satellite beside other actuators like reaction wheel or thruster.

It also can be used for unloading reaction wheels and as main actuator in detumbling phase.

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Cold Gas Thruster SAV-TCG110

After placing the satellite in orbit, the most important mission is to control its attitude.
Cold gas thruster is one of the important elements in the satellite attitude control system and it is used for stability in attitude control, orbit correction or change in the orbit of the wheel around the earth.

A SAVomid Cold Gas Thruster is a propulsive device that uses pressurized inert gas as the reaction mass. The compressed gas is released through a propelling nozzle to generate a cold jet thrust.

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Magnetometer SAV-SMM110

SAV-SMM110 designed to measure the external magnetic field vector for satellite attitude determination and control.

An integrated set of orthogonally arranged Anisotropic-Magneto-resistive (AMR) sensors provides x-, y- and z-axes magnetic field measurements.

A temperature sensor for internal temperature compensation and temperature monitoring is integrated into the magnetometer. All communication between the user and the instrument, as well as all internal controlling is handled by an 8 bit microcontroller.

The output is linear proportional to the applied external magnetic field.

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Star Tracker

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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Integrated ADCS

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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X-Band Transmitter

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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L-Band Transmitter

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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S-Band Transmitter

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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UHF Transmitter/ VHF Receiver

Lithium-ion cells represent state-of-the-art technology yet require careful treatment over mission time. Therefore, this Battery Monitoring Unit specifically designed to meet tough requirements of precision monitoring, protecting and balancing battery packs up to 12 cells. Monitoring all internal parameters continuously through the communication interface ensures reliability and safety even in the case of failure conditions.

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