17. Peculiarities of Design and Development Test of Dispenser Turning Actuator System for SHM with Iridium NEXT SC
Organization:
Yangel Yuzhnoye State Design Office, Dnipro, Ukraine
Page: Kosm. teh. Raket. vooruΕΎ. 2017 (1); 107-110
Language: Russian
Annotation: The article presents briefly the peculiarities of designing and ground development testing of dispensers turn drive system, the system composition and functioning principle are described.
Key words:
Bibliography:
1. Mikhailov V. S. Space Dnepr. Notes on Conversion Space Rocket Program. Pushkino, 2015. 156 p.
2.Β http://kosmotras.ru.
3. Gontarovsky V. A., Makarenko A. A., Shevtsov E. I. Role and Place of Functional Tests in Development of Strategic Missile Systems. Space Technology. Missile Armaments: Collection of Scientific-technical articles. 2014. Issue 1. 164 p.
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