Single Impulse Deorbit from an Elliptical Orbit |
| Description: | Calculates the single impulsive deorbit maneuver required to establish a reentry altitude and flight path angle relative to a non-rotating, spherical Earth. The algorithm uses a tangential delta-v applied opposite to the velocity vector of an initial elliptical orbit to establish the de-orbit trajectory. |
| Filename: | edeorbit.zip |
| ID: | 9475 |
| Author: | C. Deagle, Jr. |
| Downloaded file size: | 345,225 bytes |
| Size on calculator: | 25 KB |
| Platforms: | Prime |
| User rating: | Not yet rated (you must be logged in to vote) |
| Primary category: | Science |
| Languages: | ENG |
| File date: | 2022-11-14 08:45:35 |
| Creation date: | 2022-11-24 |
| Source code: | Included |
| Download count: | 100 |
| Version history: | 2023-05-29: Added to site
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| Archive contents: | Length Date Time Name
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367097 2012-11-24 07:59 deorbit.pdf
25228 2022-11-14 05:19 edeorbit.hpprgm
2923 2022-11-14 09:45 edeorbit.html
12115 2022-11-14 05:20 edeorbit.txt
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407363 4 files |
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