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Early Program Development presented by Gerhard Heller of Marshall Space Flight Center's Research Projects Division

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Summary

As presented by Gerhard Heller of Marshall Space Flight Center's Research Projects Division in 1961, this chart illustrates three basic types of electric propulsion systems then under consideration by NASA. The ion engine (top) utilized cesium atoms ionized by hot tungsten and accelerated by an electrostatic field to produce thrust. The arc engine (middle) achieved propulsion by heating a propellant with an electric arc and then producing an expansion of the hot gas or plasma in a convergent-divergent duct. The electromagnetic, or MFD engine (bottom) manipulated strong magnetic fields to interact with a plasma and produce acceleration.

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electric msfc marshall space flight center program development gerhard heller arc engine field plasma ion engine mfd engine propulsion systems program development propulsion cesium atoms arc convergent divergent duct nasa
date_range

Date

01/01/1961
place

Location

Marshall Spaceflight Center, Huntsville, Madison County, Alabama, United States, 35808 ,  34.63076, -86.66505
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Source

NASA
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Link

https://images.nasa.gov/
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Public Domain Dedication (CC0)

label_outline Explore Ion Engine, Propulsion Systems, Program Development

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electric msfc marshall space flight center program development gerhard heller arc engine field plasma ion engine mfd engine propulsion systems program development propulsion cesium atoms arc convergent divergent duct nasa