Výsledky vyhledávání - "Bowles, Jeffrey V."

This thesis describes a number of issues associated with waverider configured spacecraft designed for interplanetary missions. The first such issue is the determination of the magnitude of the energies and velocities required for conventional gravity

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______2778::c6b57a9a8768fc3a08b30e041309dead
https://hdl.handle.net/10945/32074

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Low-speed wind tunnel testing of the NPS/NASA Ames Mach 6 optimized waverider

Autor: Cedrun, Mark E.

Low-speed wind tunnel tests were conducted to determine the subsonic aerodynamic characteristics of an optimized supersonic (Mach 6) conical-flow waverider designed for a deck-launched intercept mission. These tests are part of the continuing waverid

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______2778::4d17d4acf7f06b08abf75a0223980c13
https://hdl.handle.net/10945/30832

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Optimization and performance analysis of a supersonic conical-flow waverider for a deck-launched intercept mission

Autor: Price, David R.

An aircraft configuration for a deck launched intercept mission was investigated. The mission requirements for the carrier-launched and recovered aircraft included Mach 6 cruise out to a 1000 nautical mile combat radius and 20 minutes of combat follo

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______2778::9bc333f433f8c6de65eb84e90b9ffb9e
https://hdl.handle.net/10945/39832

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