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of 4
pro vyhledávání: '"Francesco Maria Marin"'
Numerical Prediction of Internal Flows in He/LOx Seals for Liquid Rocket Engine Cryogenic Turbopumps
Autor:
Lorenzo Maritano, Francesco Maria Marin, Cristina Bertani, Dario Pastrone, Maddalena Angelucci, Giuseppe Caggiano
Publikováno v:
Applied Sciences, Vol 12, Iss 21, p 10776 (2022)
Cryogenic turbopumps are used in high-performance, lightweight liquid rocket engines for space applications. The development of bearings and shaft seals for cryogenic turbopumps requires detailed characterization of the internal flow, taking into acc
Externí odkaz:
https://doaj.org/article/ba48043452ab404b8c81ce0d9b87307a
Autor:
Lorenzo Mazzei, Francesco Maria Marin, Cosimo Bianchini, Riccardo Da Soghe, Cristina Bertani, Dario Pastrone, Maddalena Angelucci, Giuseppe Caggiano, Michiel de Beer
Publikováno v:
Fluids, Vol 7, Iss 2, p 42 (2022)
Cryogenic liquid propellants are used in liquid rocket engines to obtain high specific impulse. The flow rates are controlled by turbopumps that deliver liquid propellant to the engine at high pressure levels. Due to the very low saturation temperatu
Externí odkaz:
https://doaj.org/article/1cce3fea5f9d4ea996f4c5f5d9c44d6c
Publikováno v:
Frontiers in Genetics, Vol 13 (2022)
Externí odkaz:
https://doaj.org/article/f6d6ae09f6464651aa332ea5a1c0e5f1
Autor:
Lorenzo Mazzei, Francesco Maria Marin, Cosimo Bianchini, Riccardo Da Soghe, Cristina Bertani, Dario Pastrone, Maddalena Angelucci, Giuseppe Caggiano, Michiel de Beer
Publikováno v:
Fluids; Volume 7; Issue 2; Pages: 42
Fluids, 7(2):42. Multidisciplinary Digital Publishing Institute (MDPI)
Fluids, 7(2):42. Multidisciplinary Digital Publishing Institute (MDPI)
Cryogenic liquid propellants are used in liquid rocket engines to obtain high specific impulse. The flow rates are controlled by turbopumps that deliver liquid propellant to the engine at high pressure levels. Due to the very low saturation temperatu