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| Description |
Saturn V dynamic testing was conducted in three configurations:
Configuration I simulates the flight vehicle configuration during the first phase of flight, when the first stage, S-IC provides thrust, and is made up of the S-IC-D, the S-II-S/D, the S-IVB-D stages, the S-IU-200D/500D instrument unit and the BP-027 spacecraft. Configuration II simulates the flight vehicle configuration during the second phase of flight, when the second stage, S-II provides thrust, and is made up of the S-II-S/D, S-IVB-D, the S-IU-200D/500D and the BP-27. Configuration III simulates the flight vehicle configuration during the third phase of flight, when the third stage, S-IVB provides thrust, and is made up of S-IVB-D, the S-IU-200D/500D and the BP-27. |
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| Date | ||||||
| Source | [1] | |||||
| Author | NASA | |||||
| Permission (Reusing this file) |
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| current | 02:43, 30 March 2011 | | 601 × 768 (26 KB) | Ke4roh | {{Information |Description ={{en|1=Saturn V dynamic testing was conducted in three configurations: '''Configuration I''' simulates the flight vehicle configuration during the first phase of flight, when the first stage, S-IC provides thrust, and is ma |
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