Winged rocket performance analysis
A method is presented for estimating the effects of various parameters on the performance of a winged rocket. A program for studying three specific parameters, i.e., wing areas, reduced thrust cruising programs, and trajectory climb angles, and their effect on the horizontal range of a winged rocket...
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Format: | Others |
Published: |
1949
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Online Access: | https://thesis.library.caltech.edu/511/1/Shonerd_de_1949.pdf Shonerd, David E. (1949) Winged rocket performance analysis. Engineer's thesis, California Institute of Technology. doi:10.7907/34ZH-KG02. https://resolver.caltech.edu/CaltechETD:etd-02052009-092504 <https://resolver.caltech.edu/CaltechETD:etd-02052009-092504> |
Internet
https://thesis.library.caltech.edu/511/1/Shonerd_de_1949.pdfShonerd, David E. (1949) Winged rocket performance analysis. Engineer's thesis, California Institute of Technology. doi:10.7907/34ZH-KG02. https://resolver.caltech.edu/CaltechETD:etd-02052009-092504 <https://resolver.caltech.edu/CaltechETD:etd-02052009-092504>