Early Program Development presented by Gerhard Heller of Marshall Space Flight Center's Research Projects Division
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.
Nothing Found.
Tags
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
01/01/1961
Location
Marshall Spaceflight Center, Huntsville, Madison County, Alabama, United States, 35808
,
34.63076, -86.66505
Source
NASA
Link
Copyright info
Public Domain Dedication (CC0)