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Titel:

Design of Open-End Liquid-Liquid Bi-Swirl Coaxial Injectors for Transcritical Injection in an Oxidizer-Rich Preburner

Dokumenttyp:
Konferenzbeitrag
Autor(en):
Polidar, A., Mair, M., Abplanalp, D., Brieschenk, S., Manfletti, C.
Stichworte:
transcritical injection, liquid-liquid bi-propellant rocket engine, preburner, model-based design, additive manufacturing, oxidizer-rich staged combustion
Kongress- / Buchtitel:
Space Propulsion 2022
Jahr:
2022
Jahr / Monat:
2022-05
WWW:
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