Derated ion thruster design issues
Michael J. Patterson
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Derated ion thruster design issues
Published
1991
Publisher
National Aeronautics and Space Administration
Pages
1
Subjects
Fundamentals of Electric Propulsion
Ion propulsion for space flight
Fundamentals of electric propulsion
Characterization of 8-cm engineering model thruster
High-power ion thruster technology
5-kW xenon ion thruster lifetest
Frequently Asked Questions
How many pages are in Derated ion thruster design issues?
This edition of Derated ion thruster design issues has approximately 1 pages. Please note, this is an estimate and the exact page count can vary between hardcover, paperback, and e-book versions.
How long does it take to read Derated ion thruster design issues?
For most readers, Derated ion thruster design issues typically takes between 1m and 1m to complete. This is based on the book's length of approximately 250 words and common reading speeds.
Here's a detailed breakdown: • Continuous reading at 250 WPM: approximately 1m of focused reading • Casual reading (30 minutes/day): you could finish in roughly 1 day • Estimated word count: 250 words
Your individual reading time will vary based on your personal reading pace, the amount of daily reading time, and your familiarity with the subject matter.
What is the word count of Derated ion thruster design issues?
The estimated word count for Derated ion thruster design issues is approximately 250 words. This figure is calculated using industry-standard methods that consider genre-specific word density patterns, typical formatting and layout characteristics, and standard words-per-page ratios for published books.
This is an approximation — actual word count may vary based on font size, formatting, edition, and the presence of illustrations or charts.
Who is the author of Derated ion thruster design issues?
Derated ion thruster design issues was written by Michael J. Patterson.
When was Derated ion thruster design issues published?
The publication date for this specific edition is 1991. The original work may have been published on a different date.