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1

External thermal modeling satellite platform «Synergy»

O.Ya. Yakovlev, D.V. Malygin

275

2

Design of the mirror antenna of a spacecraft with the ultralight high precision size-stable reflector

V.B. Taygin, А.V. Lopatin

251

3

Analysis of design of spacecraft solar arrays

Z.A. Kazantsev, A.M. Eroshenko, L.A. Babkina, A.V. Lopatin

244

4

Attitude control and determination algorithms for the spacecraft with two flexible appendages

D.S. Ivanov, S.V. Meus, A.B. Nuralieva, A.V. Ovchinnikov, M.Yu. Ovchinnikov, D.S. Roldugin, S.S. Tkachev, A.I. Shestoperov, S.A. Shestakov, E.N. Yakimov

240

5

Calculation and experimental assessment of the strength and limit states of composite structures for spacecraft

V.V. Moskvichev, A.M. Lepikhin, A.E. Burov, S.V. Doronin, E.V. Moskvichev

239

6

Method of achievement the high accuracy of the shape of reflectors of mirror antennas of spacecraft

V.B. Taygin, А.V. Lopatin

238

7

The main directions of research and development of BSTU «VOENMEH» named after D. F. Ustinov on the subject of small spacecraft and some results

M.I. Kislitsky

237

8

Software package «Integral» for modeling space constellations and space vehicles

N.A. Zavialova, S.S. Negodyaev, A.A. Kuznetsov, I.N. Zavialov, I.I. Fukin, V.Yu. Semaka, P.A. Grishin

235

9

Mathematical modeling of piezoelectric step-engine work

A.V. Azin, S.A. Kuznetsov, S.A. Ponomarev, S.V. Ponomarev, S.V. Rikkonen

228

10

Optimization of the structure of the unified multichannel interface temperature control module for measuring instruments of spacecraft

A.I. Gornostaev

227