NEXT 6.9 kW Ion Thruster
Overview
The NEXT 6.9 kW Ion Thruster is an Electric Propulsion Thruster developed by Aerojet Rocketdyne. Aerojet Rocketdyne's is designed for SmallSat with a mass of 13.3 kg and an average power consumption of 3750 W.
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Overview
- Name
- NEXT 6.9 kW Ion Thruster
- Vendor
- Aerojet Rocketdyne
- Subsystem
- Propulsion Subsystem
- Component Type
- Electric Propulsion Thruster
- Form Factor
- SmallSat
- Heritage
- N/A
Vendor Details
- Name
- Aerojet Rocketdyne
- Website
- https://www.rocket.com/
- Founded
- 1942
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Specifications
- Subsystem
- Propulsion Subsystem
- Component Type
- Electric Propulsion Thruster
- Form Factor
- SmallSat
- Vendor
- Aerojet Rocketdyne
- Dry Mass
- 13.3 kg
- Average Power
- 3,750.0 W
- Heritage
- N/A
- Status
- In Production
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Aerojet Rocketdyne
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