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- W1998164900 abstract "Technical limitations and requirements on the state of the test gas suggest accelerating models rather than accelerating the test gas for hypervelocity testing. This holds particularly for measuring methods that necessitate longer measurement times, such as force or heating measurements, or investigation s of propulsion, ablation, or re-entry in nonterrestrial atmospheres. Conveniently, recent developments in instrumentation, on-board data transmission and recording, and acceleration techniques extend the capability of free-flight experiments. In addition to general considerations, this article gives an example of the outline of a suitable test facility based on the ram accelerator hypervelocity launcher concept and its adaptation to different measuring tasks." @default.
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- W1998164900 date "1994-11-01" @default.
- W1998164900 modified "2023-10-18" @default.
- W1998164900 title "Ram accelerator ballistic range concept for softly accelerating hypersonic free-flying models" @default.
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- W1998164900 doi "https://doi.org/10.2514/3.46652" @default.
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