A study was conducted of a three-engined external hydrogen tank orbiter/heat sink booster utilizing 415 K sea level thrust engines. The results of the study, pertaining to the orbiter portion of the configuration, are presented. A complete summary of characteristics is given for the external tank configuration along with some comparative data for a conventional internal tank configuration.
Alternate Space Shuttle Concepts Study. Part 2 Technical Summary. Volume 2 Orbiter Definition
1971
431 pages
Report
Keine Angabe
Englisch
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