File:Apollo17 Ascent Trajectory.pdf
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DescriptionApollo17 Ascent Trajectory.pdf |
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.http://www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue |
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 17:50, 6 January 2019 | 1,752 × 1,239 (64 KB) | WG14159 (talk | contribs) | Added the table "Saturn V Staging Parameters" | |
21:05, 29 February 2016 | No thumbnail | 0 × 0 (89 KB) | WG14159 (talk | contribs) | {{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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Author | Grimm, Wolfgang |
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Software used | Acrobat PDFMaker 18 für Excel |
Conversion program | Adobe PDF Library 15.0 |
Encrypted | no |
Page size | 841.68 x 595.2 pts |
Version of PDF format | 1.5 |