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1

External thermal modeling satellite platform «Synergy»

O.Ya. Yakovlev, D.V. Malygin

276

2

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

V.B. Taygin, А.V. Lopatin

255

3

Analysis of design of spacecraft solar arrays

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

246

4

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

243

5

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

242

6

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

V.B. Taygin, А.V. Lopatin

241

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

The satellite distance radiometer with a passive retroreflection of a request radio signal

V.E. Chebotarev, Yu.P. Salomatov, V.S. Panko, A.A. Erokhin, E.V. Kuzmin, R.O. Ryazantsev

233

10

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

A.I. Gornostaev

230