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, Zenzerov V. I., Zenzerov V. I., Zenzerov V. I., Zenzerov V. I., Zenzerov V. I., Zenzerov V. I., Zenzerov V.
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2. Experience of Testing SRM Thrust Vector Controls

Authors:

Golubenko M. S., Kushnir B. I., Zenzerov V. O.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2016 (1); 13-18

Language: Russian

Annotation: The design peculiarities and basic characteristics of thrust vector controls of main SRM developed by Yuzhnoye SDO DO-5 beginning from 1966 are presented. The basic design and design-theoretical problems solved during thrust vector controls development are considered.

Key words:

Bibliography:

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2.1.2016 Experience of Testing SRM Thrust Vector Controls
2.1.2016 Experience of Testing SRM Thrust Vector Controls
2.1.2016 Experience of Testing SRM Thrust Vector Controls
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