Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Vito Salvatore"'
Publikováno v:
Scopus-Elsevier
Human and robotic exploration is foreseen to be one of the next steps in human space colonization, and it is growing the common vision that Moon, on the pathway to Mars, is the outpost to extend human presence in deep space. At the same time, technol
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c8ba83933db49339777b99284df32453
https://doi.org/10.1007/s42496-019-00008-3
https://doi.org/10.1007/s42496-019-00008-3
Autor:
Giuseppe Leccese, Francesco Battista, Vito Salvatore, Scott E. Meyer, Raffaele Votta, Francesco Nasuti, Marco Pizzarelli
Publikováno v:
Applied Thermal Engineering. 101:61-70
A test article has been specifically designed in order to investigate the methane behaviour inside rocket engine cooling channels. The test article is composed of a suitable copper-alloy block warmed up by cartridge heaters and of a single channel wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a8db4ed1ec343f219cb806e70077d1f8
https://doi.org/10.1016/j.applthermaleng.2015.12.019
https://doi.org/10.1016/j.applthermaleng.2015.12.019
Publikováno v:
Volume 1: Advances in Aerospace Technology.
The HYPROB Program, led by the Italian Aerospace Research Centre, has the aim to increase the Italian capabilities in the design and manufacture of liquid oxygen-methane rocket engines; in particular, the line, named HYPROB-BREAD, has the final goal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36242a6c75c7d091457480bb25473777
https://doi.org/10.1115/imece2015-51625
https://doi.org/10.1115/imece2015-51625
Publikováno v:
Volume 1: Advances in Aerospace Technology.
The HYPROB Program, developed by the Italian Aerospace Research Centre, has the aim of increasing the Italian system design and manufacturing capabilities on liquid oxygen-hydrocarbon rocket engines; the most important activity is represented by the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d04ea4fb8724055f5875131c5adfce07
https://doi.org/10.1115/imece2015-51554
https://doi.org/10.1115/imece2015-51554
Publikováno v:
Volume 1: Advances in Aerospace Technology.
The HYPROB Program, developed by the Italian Aerospace Research Centre, has the aim to increase the system design and manufacturing capabilities on liquid oxygen-methane rocket engines. It foresees the designing, manufacturing and testing of a ground
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9125bad10bcf6b0bb08e2167ec59f916
https://doi.org/10.1115/imece2014-36998
https://doi.org/10.1115/imece2014-36998
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Liquid rocket engine development using oxygen and methane propellants is currently underway at CIRA within the context of the Hyprob program funded by the Italian Ministry of University and Research (MIUR). Different methods for evaluating the perfor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8f74cfcdb6ed0e97a9b83fac9571146a
https://doi.org/10.2514/6.2014-3985
https://doi.org/10.2514/6.2014-3985
Autor:
Daniele Ricci, Francesco Battista, Barbara Betti, Pietro Roncioni, Marco Pizzarelli, Vito Salvatore, Francesco Nasuti
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
A computational procedure able to describe the coupled hot-gas/wall/coolant environment that occurs in most liquid rocket engines is presented and demonstrated. The coupled analysis is performed by loose coupling of the two-dimensional axisymmetric R
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d062c8e12c0f407f55ee0c39eb1ceda3
https://doi.org/10.2514/6.2014-4004
https://doi.org/10.2514/6.2014-4004
Autor:
A. Gianvito, Vito Salvatore, S. Shark, A. Smoraldi, Raffaele Votta, Marco Pizzarelli, Francesco Nasuti, Giuseppe Leccese, Francesco Battista, R. Feddema, Scott E. Meyer
The use of the Methane as coolant in a regenerative liquid rocket engine (LRE) presents some difficulties since transcritical fluidynamics operating conditions occur in the cooling channels. Transcritical conditions cause large fluid properties varia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c25e0060f4abef1beb559e641da39f56
http://hdl.handle.net/11573/626610
http://hdl.handle.net/11573/626610
Autor:
Michele Ferraiuolo, Francesco Battista, Pierpaolo De Matteis, Pietro Roncioni, Vito Salvatore, Raffaele Votta
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The use of the Methane as coolant in a regenerative liquid rocket engine (LRE) presents some difficulties since transcritical fluidynamics operating conditions occur in the cooling channels. Transcritical conditions cause large fluid properties varia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8ea0e66370c4e3bdc9802e03e318387b
https://doi.org/10.2514/6.2013-4146
https://doi.org/10.2514/6.2013-4146