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Evaluation of Aerodynamic Drag and Torque for External Tanks in Low Earth Orbit
A numerical procedure is described in which the aerodynamic drag and torque in low Earth orbit are calculated for a prototype Space Shuttle external tank and its components, the “LO2” and “LH2” tanks, carrying liquid oxygen and hydrogen, respectively, for any given angle of attack. Calculations assu...
| Autores principales: | , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
[Gaithersburg, MD] : U.S. Dept. of Commerce, National Institute of Standards and Technology
2006
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| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4662504/ https://www.ncbi.nlm.nih.gov/pubmed/27274926 http://dx.doi.org/10.6028/jres.111.014 |