File:Optimal Transfer Orbit using Electric Propulsion.png
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Size of this preview: 784 × 599 pixels. Other resolutions: 314 × 240 pixels | 628 × 480 pixels | 849 × 649 pixels.
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Summary
| Description |
English: Sequence and method of translating a satellite from an eliptical supersynchronous to the geosynchronous orbit using electric proulsion |
| Date | |
| Source | Own work |
| Author | Arnonspitzer |
Licensing
I, the copyright holder of this work, hereby publish it under the following license:
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 13:28, 22 June 2015 | | 849 × 649 (30 KB) | wikimediacommons>Arnonspitzer | User created page with UploadWizard |
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