ROCKET 168 SLOT：Effects of slot throat width on two-phase n-decane/air rotating

rocket 168 slot   game rocket slot The converging–diverging inlet configuration with various slot throat widths 0.5, 1.0, 1.5, and 2.0 mm is considered. The influence of slot throat width on the flow field structures, pressure feedback, total pressure gain, and theoretical model of a design parameter L/h D for the rotating detonation chamber RDC are discussed. The

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a rocket to the moon The Artemis II test flight will be NASA’s first mission with crew aboard the SLS Space Launch System rocket and Orion spacecraft and will pave the way to land astronauts on the Moon on Artemis III. Artemis II builds on the success of the uncrewed Artemis I mission and will demonstrate a broad range of capabilities needed on lunar missions