Centaur/Shuttle Integration and Operations
1971
- 301Usage
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
Citation Benchmarking is provided by Scopus and SciVal and is different from the metrics context provided by PlumX Metrics.
Metrics Details
- Usage301
- Downloads286
- Abstract Views15
Artifact Description
One of the major pay loads to be considered for delivery to orbit by the Space Shuttle is a cryogenic propulsion stage.An investigation was conducted, in conjunction with North American Rockwell, to investigate the interfaces between the Centaur and the Shuttle and the various possible operational modes of launching the Centaur in the Shuttle, The Centaur vehicle was used as the design model since its characteristics are presently well defined and it accommodates all the unmanned missions in the time period of interest.The results of the study showed Centaur integration into the Space Shuttle to be feasible with minimum additional GSE and operational complexity.
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