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Control of angular motion of a landing module of “Soyuz” type upon satellite returning from the orbit

✍ Scribed by S. N. Evdokimov; S. I. Klimanov; L. I. Komarova; E. A. Mikrin


Book ID
111454019
Publisher
SP MAIK Nauka/Interperiodica
Year
2011
Tongue
English
Weight
563 KB
Volume
50
Category
Article
ISSN
1064-2307

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