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18 results on '"Becatti, G"'

4. U-PHOS EXPERIMENT: THERMAL RESPONSE OF A LARGE DIAMETER PULSATING HEAT PIPE ON BOARD REXUS 22 ROCKET

Author

Catarsi, A., Anichini, M., Barsocchi, L., Becatti, G., Buoni, L., Celi, F., Di Giorgio, P., Fattibene, P., Guardati1, E. Ferrato P., Mancini, E., Meoni, G., Nannipieri, P., Nesti, F., Piacquadio, S., Pratelli, E., Quadrelli, L., Viglione, A. S., Zanaboni, F., Mameli, M., Baronti, F., Fanucci, L., Marcuccio, S., Bartoli, C., Di Marco, P., Filippeschi, S., Bianco, N., and Marengo, M.

Published
2017

5. U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22

Author

Nannipieri, P, primary, Anichini, M, additional, Barsocchi, L, additional, Becatti, G, additional, Buoni, L, additional, Celi, F, additional, Catarsi, A, additional, Di Giorgio, P, additional, Fattibene, P, additional, Ferrato, E, additional, Guardati, P, additional, Mancini, E, additional, Meoni, G, additional, Nesti, F, additional, Piacquadio, S, additional, Pratelli, E, additional, Quadrelli, L, additional, Viglione, A S, additional, Zanaboni, F, additional, Mameli, M, additional, Baronti, F, additional, Fanucci, L, additional, Marcuccio, S, additional, Bartoli, C, additional, Di Marco, P, additional, Bianco, N, additional, Marengo, M, additional, and Filippeschi, S, additional

Published
2017
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9. Pulsating Heat pipe Only for Space (PHOS): results of the REXUS 18 sounding rocket campaign

Author

Creatini, F, primary, Guidi, G M, additional, Belfi, F, additional, Cicero, G, additional, Fioriti, D, additional, Di Prizio, D, additional, Piacquadio, S, additional, Becatti, G, additional, Orlandini, G, additional, Frigerio, A, additional, Fontanesi, S, additional, Nannipieri, P, additional, Rognini, M, additional, Morganti, N, additional, Filippeschi, S, additional, Marco, P Di, additional, Fanucci, L, additional, Baronti, F, additional, Mameli, M, additional, Manzoni, M, additional, and Marengo, M, additional

Published
2015
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10. HT20k Hall Thruster development status

Author

Andreussi, T., ANTONIO PIRAGINO, Ferrato, E., Reza, M., Faraji, F., Becatti, G., Pedrini, D., Kitaeva, A., Rossodivita, A., and Andrenucci, M.

11. U-PHOS EXPERIMENT: THERMAL RESPONSE OF A LARGE DIAMETER PULSATING HEAT PIPE ON BOARD REXUS 22 ROCKET

Author

ESA, Catarsi, A., Anichini, M., Barsocchi, L., Becatti, G., Buoni, L., Celi, F., Di Giorgio, P., Fattibene, P., Guardati, E. Ferrato P., Mancini, E., Meoni, G., Nannipieri, P., Nesti, F., Piacquadio, S., Pratelli, E., Quadrelli, L., Viglione, A. S., Zanaboni, F., mauro mameli, Federico Baronti, Luca Fanucci, SALVO MARCUCCIO, CARLO BARTOLI, Paolo Di Marco, Sauro Filippeschi, Bianco, N., and Marengo, M.

12. U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22

Author

Organizing Committee, Nannipieri, P., Anichini, M., Barsocchi, L., Becatti, G., Buoni, L., Celi, F., Catarsi, A., Di Giorgio, P., Fattibene, P., Ferrato, E., Guardati, P., Mancini, E., Meoni, G., Nesti, F., Piacquadio, S., Pratelli, E., Quadrelli, L., Viglione, A. S., Zanaboni, F., mauro mameli, Federico Baronti, Luca Fanucci, SALVO MARCUCCIO, CARLO BARTOLI, Paolo Di Marco, Bianco, N., Marengo, M., and Sauro Filippeschi

14. Upgraded Pulsating Heat Pipe Only For Space (U-Phos): Results of the 22nd Rexus Sounding Rocket Campaign

Author

Nannipieri, P., Anichini, M., Barsocchi, L., Becatti, G., Buoni, L., Celi, F., Catarsi, A., Di Giorgio, P., Fattibene, P. Ferrato E., Guardati, P., Mancini, E., Meoni, G., Nesti, F., Piacquadio, S., Pratelli, E., Quadrelli, L., Viglione, A. S., Zanaboni, F., mauro mameli, Federico Baronti, Luca Fanucci, SALVO MARCUCCIO, CARLO BARTOLI, Paolo Di Marco, Bianco, N., and Sauro Filippeschi

Subjects
Sounding Rocket, Large Diameter Pulsating Heat Pipe, Sounding Rocket, Milligravity, Milligravity, Large Diameter Pulsating Heat Pipe

17. U-PHOS Project: Development of a Large Diameter Pulsating Heat Pipe Experiment on board REXUS 22

Author

Gabriele Meoni, Sauro Filippeschi, Federico Baronti, Pietro Guardati, A. Catarsi, L. Buoni, Alessandro Simone Viglione, Salvo Marcuccio, Carlo Bartoli, L. Barsocchi, P. Fattibene, E. Pratelli, Federico Celi, Eugenio Ferrato, Lorenzo Quadrelli, S. Piacquadio, Federico Nesti, F. Zanaboni, Marco Marengo, G. Becatti, M. Anichini, Mauro Mameli, Luca Fanucci, P. Di Giorgio, Edoardo Mancini, P. Di Marco, Pietro Nannipieri, Nicola Bianco, Nannipieri, P, Anichini, M, Barsocchi, L, Becatti, G, Buoni, L, Celi, F, Catarsi, A, Di Giorgio, P, Fattibene, P, Ferrato, E, Guardati, P, Mancini, E, Meoni, G, Nesti, F, Piacquadio, S, Pratelli, E, Quadrelli, L, Viglione, A. S, Zanaboni, F, Mameli, M, Baronti, F, Fanucci, L, Marcuccio, S, Bartoli, C, Di Marco, P, Bianco, Nicola, Marengo, M, and Filippeschi, S.

Subjects
History, Engineering drawing, Materials science, Sounding rocket, Buoyancy, 020209 energy, Mechanical engineering, 02 engineering and technology, engineering.material, Phase-change material, Pressure sensor, Computer Science Applications, Education, Physics and Astronomy (all), Heat pipe, 020401 chemical engineering, 0202 electrical engineering, electronic engineering, information engineering, engineering, Tube (fluid conveyance), 0204 chemical engineering, Condenser (heat transfer), Evaporator
Abstract

U-PHOS Project aims at analysing and characterising the behaviour of a large diameter Pulsating Heat Pipe (PHP) on board REXUS 22 sounding rocket. A PHP is a passive thermal control device where the heat is efficiently transported by means of the self-sustained oscillatory fluid motion driven by the phase change phenomena. Since, in milli-gravity conditions, buoyancy forces become less intense, the PHP diameter may be increased still maintaining the slug/plug typical flow pattern. Consequently, the PHP heat power capability may be increased too. U-PHOS aims at proving that a large diameter PHP effectively works in milli-g conditions by characterizing its thermal response during a sounding rocket flight. The actual PHP tube is made of aluminum (3 mm inner diameter, filled with FC-72), heated at the evaporator by a compact electrical resistance, cooled at the condenser by a Phase Change Material (PCM) embedded in a metallic foam. The tube wall temperatures are recorded by means of Fibre Bragg Grating (FBG) sensors; the local fluid pressure is acquired by means of a pressure transducer. The present work intends to report the actual status of the project, focusing in particular on the experiment improvements with respect to the previous campaign.

Published
2017

18. Compact scanning retarding potential analyzer.

Author

Goebel DM and Becatti G

Abstract

A miniature scanning electrostatic energy analyzer has been developed for measurements of the ion energy distribution in low-pressure plasma discharges. The retarding potential analyzer utilizes four grids to reject the incident electron flux and discriminate the ion energy. It features a compact size of 5-mm diameter and 2.5-mm thickness and uses a simple configuration to mount the grids and provide voltage isolation using high temperature ceramic cement that avoids complicated grid alignment or MEMS fabrication techniques. Mounting on a fast-scanning two-axis probe drive eliminates overheating of the ceramics and subsequent current leakage, which permits insertion into challenging locations and provides profiles of the ion energy in the plasma discharge. Guidelines for the analyzer design for high density operation are discussed, and the performance of the analyzer is shown for measurements in a hollow cathode plume in xenon plasmas.

Published
2021
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