Summary

The Nakashimada Engineering Works De-Orbit Mechanism is designed for LEO applications for satellites ranging between 1U to 50 kg.

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Last updated: 2022-04-13

Nakashimada Engineering Works, Ltd.

DOM - De-Orbit Mechanism

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DOM - De-Orbit Mechanism

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from our blog

Find a launch option for your CubeSat or small satellite - an overview of launch service providers

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Optical communications for small satellites and CubeSats - product roundup

Satellite > Orbit Determination and Control > De-orbiting device > DOM - De-Orbit Mechanism

DOM - De-Orbit Mechanism

Submit your request

Request details

Personal Information

Submitting your information allows us to get in touch with you once we get a response from the supplier.

from our blog

Find a launch option for your CubeSat or small satellite - an overview of launch service providers

Smallsat and CubeSat GPS antennas and GNSS systems

Optical communications for small satellites and CubeSats - product roundup