Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom

Method and arrangement for reducing the effects of a some boom created by an aerospace vehicle when said vehicle is flown at supersonic speed. The method includes providing the aerospace vehicle with a first spike extending from the nose thereof substantially in the direction of normal flight of the...

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Bibliographische Detailangaben
Hauptverfasser: HOWE DONALD C, HENNE PRESTON A
Format: Patent
Sprache:eng
Schlagworte:
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