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Laboratory Model 50 KW Hall Thruster

National Aeronautics and Space Administration
4.9/5 (12967 ratings)
Description:A 0.46 meter diameter Hall thruster was fabricated and performance tested at powers up to 72 kilowatts. Thrusts up to 2.9 Newtons were measured. Discharge specific impulses ranged from 1750 to 3250 seconds with discharge efficiencies between 46 and 65 percent. Overall specific impulses ranged from 1550 to 3050 seconds with overall efficiencies between 40 and 57 percent. Performance data indicated significant fraction of multiple-charged ions during operation at elevated power levels. Cathode mass flow rate was shown to be a significant parameter with regard to thruster efficiency. Manzella, David and Jankovsky, Robert and Hofer, Richard Glenn Research Center NASA/TM-2002-211887, NAS 1.15:211887, E-13569, AIAA Paper 2002-3676We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Laboratory Model 50 KW Hall Thruster. To get started finding Laboratory Model 50 KW Hall Thruster, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
32
Format
PDF, EPUB & Kindle Edition
Publisher
Createspace Independent Publishing Platform
Release
2018
ISBN
1721530649

Laboratory Model 50 KW Hall Thruster

National Aeronautics and Space Administration
4.4/5 (1290744 ratings)
Description: A 0.46 meter diameter Hall thruster was fabricated and performance tested at powers up to 72 kilowatts. Thrusts up to 2.9 Newtons were measured. Discharge specific impulses ranged from 1750 to 3250 seconds with discharge efficiencies between 46 and 65 percent. Overall specific impulses ranged from 1550 to 3050 seconds with overall efficiencies between 40 and 57 percent. Performance data indicated significant fraction of multiple-charged ions during operation at elevated power levels. Cathode mass flow rate was shown to be a significant parameter with regard to thruster efficiency. Manzella, David and Jankovsky, Robert and Hofer, Richard Glenn Research Center NASA/TM-2002-211887, NAS 1.15:211887, E-13569, AIAA Paper 2002-3676We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Laboratory Model 50 KW Hall Thruster. To get started finding Laboratory Model 50 KW Hall Thruster, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
32
Format
PDF, EPUB & Kindle Edition
Publisher
Createspace Independent Publishing Platform
Release
2018
ISBN
1721530649

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