10. Features of Measurement System for Gas-Dynamic Model Tests of Rocket Complex Elements
Organization:
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Page: Kosm. teh. Raket. vooruž. 2017 (1); 67-69
Language: Russian
Annotation: The design proposals for sensor equipment of the measurement system used during gas dynamic model tests of rocket systems elements are presented.
Key words:
Bibliography:
1. Cyclone-4. 21.17827.122ОТ: Report on research work / Yuzhnoye SDO. Dnipropetrovsk, 2014. P. 12.
2. Krivorotov N. P. Microelectronic Pressure Sensors / N. P. Krivorotov, Т. I. Izaak, L. M. Romas’, Y. G. Svinolupov, S. S. Shchyogol. News of Tom. State University. 2005. No. 285. P. 139-147.
3. Zhadko I. P. Silicon Pressure Transducer with Differential Sensitive Element Based on Transverse Electromotive Force Effect / I. P. Zhadko, G. G. Babichev, S. I. Kozlovskiy, V. A. Romanov, N. N. Sharan, E. A. Zinchenko. Institute of Semiconductor Physics, National Academy of Science of the Ukraine. К., 2001. 7 р.
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