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Summary
| Description |
English: Apollo 17 flight trajectory from liftoff to end of S-IVB first burn.
- Altitude is given above Fischer Ellipsoid.
- Gravity (total acceleration) is calculated according to
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| Date | |
| Source |
Own work, based on the following sources:
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19760012111.pdf
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| Author | WG14159 |
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Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. |
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 17:50, 6 January 2019 |  | 1,752 × 1,239 (64 KB) | WG14159 | Added the table "Saturn V Staging Parameters" |
| 21:05, 29 February 2016 | No thumbnail | 0 × 0 (89 KB) | WG14159 | {{Information |Description ={{en|1=- Altitude is given above Fischer Ellipsoid, e.g. EPO altitude 172km at 6:40 = 6545km geocentric distance = 167km above a spherical Earth of radius 6378.1 km - Gravity (total acceleration) was calculated according... |
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