Gas acceleration by travelling conduction waves
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Description
A theory of operation has been derived for a proposed Travelling Conduction Wave accelerator, which predicts that such a device would be capable of operating both as a medium thrust - high specific impulse space propulsion device, with round trip times to Mars of as low as one month, and as a hypersonic wind tunnel capable of simulating conditions over a major portion of the reentry corridor. A simple experiment designed to test this theory resulted in good agreement between the theory...[Show more]
Collections | Open Access Theses |
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Date published: | 1974 |
Type: | Thesis (PhD) |
URI: | http://hdl.handle.net/1885/137459 |
DOI: | 10.25911/5d70ebacecb2b |
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File | Description | Size | Format | Image |
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b10162264_Boreham_Bruce_William.pdf | 305.46 MB | Adobe PDF |
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