To develop light, reliable, sanitary space station maneuverable orbital transfer thruster, the novel gas dynamic resonance ignition method was applied.

 
  • 為研究輕型、可靠、環(huán)保的空間站機動(dòng)變軌發(fā)動(dòng)機,在氫氧液體火箭發(fā)動(dòng)機頭部設計中引入了新型氣動(dòng)諧振點(diǎn)火技術(shù)。
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