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Rotating Detonation Rocket Engine Operability Under Varied Pressure Drop Injection
Journal of Spacecraft and Rockets ( IF 1.3 ) Pub Date : 2020-09-11 , DOI: 10.2514/1.a34763 Blaine R. Bigler 1 , John W. Bennewitz 1 , Stephen A. Danczyk 1 , William A. Hargus 1
Journal of Spacecraft and Rockets ( IF 1.3 ) Pub Date : 2020-09-11 , DOI: 10.2514/1.a34763 Blaine R. Bigler 1 , John W. Bennewitz 1 , Stephen A. Danczyk 1 , William A. Hargus 1
Affiliation
Rotating detonation rocket engine (RDRE) experiments have so far been limited to injectors with high pressure drop to limit injector–plenum coupling. However, this corresponds to a reduction in the...
中文翻译:
变压降喷射下旋转爆轰火箭发动机的操作性
迄今为止,旋转爆轰火箭发动机 (RDRE) 实验仅限于具有高压降的喷射器,以限制喷射器-增压室的耦合。然而,这对应于……的减少。
更新日期:2020-09-11
中文翻译:
变压降喷射下旋转爆轰火箭发动机的操作性
迄今为止,旋转爆轰火箭发动机 (RDRE) 实验仅限于具有高压降的喷射器,以限制喷射器-增压室的耦合。然而,这对应于……的减少。