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Nasa Technical Reports Server (ntrs) 19730011096%3a Electrostatic Propulsion Beam Divergence Effects On Spacecraft Surfaces%2c Volume 2 by Nasa Technical Reports Server (ntrs)
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1NASA Technical Reports Server (NTRS) 19730011096: Electrostatic Propulsion Beam Divergence Effects On Spacecraft Surfaces, Volume 2
By NASA Technical Reports Server (NTRS)
The third phase of a program to develop understanding of and tolerance-level criteria for the deleterious effects of electrostatic rocket exhaust (Cs, Cs(+), Hg, Hg(+)) and materials of rocket construction impinging on typical classes of spacecraft (S/C) surfaces was completed. Models of ion engine effluents and models describing the degradation of S/C surfaces by these effluents are presented. Experimental data from previous phases are summarized and Phase 2 data and analysis are presented in detail. The spacecraft design implications of ion engine contaminants are discussed.
“NASA Technical Reports Server (NTRS) 19730011096: Electrostatic Propulsion Beam Divergence Effects On Spacecraft Surfaces, Volume 2” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19730011096: Electrostatic Propulsion Beam Divergence Effects On Spacecraft Surfaces, Volume 2
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19730011096: Electrostatic Propulsion Beam Divergence Effects On Spacecraft Surfaces, Volume 2” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - ELECTROSTATIC PROPULSION - ROCKET EXHAUST - SPACECRAFT STRUCTURES - CESIUM - DEGRADATION - MERCURY (METAL) - SPACECRAFT DESIGN - STATISTICAL ANALYSIS - Hall, D. F.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19730011096
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 179.35 Mbs, the file-s for this book were downloaded 72 times, the file-s went public at Mon Jul 11 2016.
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