2. Experience of Testing SRM Thrust Vector Controls

2. Experience of Testing SRM Thrust Vector Controls

Golubenko N. S., Kushnir B. I., Zenzerov V. A.

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

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.

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