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High Performance Nitrous Oxide MET, Phase I

Completed Technology Project

Project Introduction

High Performance Nitrous Oxide MET, Phase I
This proposal seeks to address the topic of developing an on-board propulsion device which will significantly increase capabilities and reduce costs for Earth science spacecraft. The propulsion device which is proposed here is a microwave powered, electrothermal thruster which will utilized nitrous-oxide as a propellant. The device is referred to a MET-100, a Microwave Electrothermal Thruster which has a nominal power output of 150 W. The thruster will utilized 300 W of spacecraft power and develop a specific impulse of 300 seconds. More »

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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.