Summary

The MMA Design dragNET™ De-Orbit System is designed for LEO applications. It consists of an efficient and highly scalable packaging along with four compactly-stowed thin membranes that release using a single heater-powered actuator.

It has a mass of 2.8 kg and is designed with the capacity to de-orbit a 180 kg spacecraft from an altitude of 850 km in less than ten years.

The product meets the requirements of the Department of Defense (DoD) as well as the National Aeronautics and Space Administration (NASA) and successfully de-orbited the ORS-3 Minotaur I Upper Stage in a two-year time frame.

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Last updated: 2022-04-13

dragNET™ De-Orbit System

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