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EtherWing's Satellite Platforms

Welcome to EC-Series Satellite Platforms

Experience the future of space exploration with EC-Series – precision-engineered platforms designed to redefine your missions.

Embark on your journey confidently with EC-12, EC-25, and EC-42, where innovation meets reliability.

Your universe awaits. Contact us to elevate your satellite projects today.

Introducing EC-Series Satellite Platforms

EC-12: Precision in a 1U CubeSat Compact and robust, EC-12 offers unmatched customization for scientific experiments and educational missions.

EC-25: Enhanced 2U CubeSat Building on EC-12's success, EC-25 provides increased payload capacity and extended power systems, redefining space missions.

EC-42: Advanced 3U CubeSat A pinnacle of innovation, EC-42 offers advanced capabilities for complex experiments and governmental missions.

Cube Sat

Form Factor

1U CubeSat

Material

6061-T6 Aluminum Alloy

Mass

1.2 kg (excluding payload)

Structure

  • Modular design with customizable payload interface.

  • Compliance with CubeSat standards (Cal Poly CubeSat Design Specification).

Communication Systems

  • UHF/VHF transceiver options (400 MHz - 450 MHz / 120 MHz - 150 MHz).

  • S-band transceiver (2.2 GHz - 2.3 GHz) or X-band transceiver (8 GHz - 12 GHz).

Power System

  • Solar panels with a total power output of up to 3W.

  • Lithium-polymer battery with configurable capacity.

Onboard Sensors

  • Slots for custom sensors (e.g., magnetometers, spectrometers).

  • Bus voltage and current sensors for real-time monitoring.

Data Handling

  • Onboard computer with an ARM Cortex-M microcontroller.

  • Customizable storage options with SPI Flash or EEPROM.

Thermal Control

  • Passive thermal management with customizable coatings.

  • Optional deployable radiators for enhanced heat dissipation.

Applications

Scientific Research

Technology Demonstration

Earth Observation

Educational Missions

EC-12

Form Factor

2U CubeSat

Material

7075-T6 Aluminum Alloy

Mass

2.5 kg (excluding payload)

Structure

  • Modular design with customizable payload interface.

  • Compliance with CubeSat standards (Cal Poly CubeSat Design Specification).

Communication Systems

  • UHF/VHF transceiver options (400 MHz - 450 MHz / 120 MHz - 150 MHz).

  • S-band transceiver (2.2 GHz - 2.3 GHz) or X-band transceiver (8 GHz - 12 GHz).

Power System

  • Solar panels with a total power output of up to 6W.

  • Lithium-polymer battery with configurable capacity.

Onboard Sensors

  • Slots for custom sensors (e.g., multispectral imaging, magnetometers).

  • Bus voltage and current sensors for real-time monitoring.

Data Handling

  • Onboard computer with an ARM Cortex-M microcontroller.

  • Customizable storage options with SPI Flash or EEPROM.

Thermal Control

  • Passive thermal management with customizable coatings.

  • Optional deployable radiators for enhanced heat dissipation.

Applications

Scientific Research

Technology Demonstration

Earth Observation

Educational Missions

EC-25

Form Factor

3U CubeSat

Material

6061-T6 Aluminum Alloy

Mass

4.2 kg (excluding payload)

Structure

  • Modular design with customizable payload interface.

  • Compliance with CubeSat standards (Cal Poly CubeSat Design Specification).

Communication Systems

  • UHF/VHF transceiver options (400 MHz - 450 MHz / 120 MHz - 150 MHz).

  • S-band transceiver (2.2 GHz - 2.3 GHz) or X-band transceiver (8 GHz - 12 GHz).

Power System

  • Solar panels with a total power output of up to 12W.

  • Lithium-polymer battery with configurable capacity.

Onboard Sensors

  • Slots for custom sensors (e.g., hyperspectral imaging, advanced magnetometers).

  • Bus voltage and current sensors for real-time monitoring.

Data Handling

  • Onboard computer with an ARM Cortex-M microcontroller.

  • Customizable storage options with SPI Flash or EEPROM.

Thermal Control

  • Passive thermal management with customizable coatings.

  • Optional deployable radiators for enhanced heat dissipation.

Applications

Scientific Research

Technology Demonstration

Earth Observation

Educational Missions

EC-42

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