Impulsive Hyperbolic Injection from a Circular Earth Orbit |
| Description: | Determines the characteristics of the single impulsive maneuver required to transfer a spacecraft from an initial circular Earth park orbit to a departure hyperbola. |
| Filename: | demo_hyper1.zip |
| ID: | 9462 |
| Author: | C. Deagle, Jr. |
| Downloaded file size: | 337,793 bytes |
| Size on calculator: | 30 KB |
| Platforms: | Prime |
| User rating: | Not yet rated (you must be logged in to vote) |
| Primary category: | Science |
| Languages: | ENG |
| File date: | 2022-09-17 04:20:28 |
| Creation date: | 2022-10-16 |
| Source code: | Included |
| Download count: | 115 |
| Version history: | 2023-05-28: Added to site
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| Archive contents: | Length Date Time Name
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30242 2022-10-16 08:05 demo_hyper1.hpprgm
3051 2022-09-17 04:20 demo_hyper1.html
14963 2022-10-16 08:04 demo_hyper1.txt
357110 2013-12-15 16:19 hyper1_matlab.pdf
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405366 4 files |
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