Archive

Volume 7, No. 3(45), 2022

Shirokov A.D., Feoktistov D.A., Oreshenko T.G., Fedorov M.S., Chubar A.V.
Verification of frequency characteristics of load devices declared by the manufacturer

181-185

Titova A.S., Sablin A.S., Zagainov M.A., Kuznetsov S.A.
Features of dynamic load analysis of spacecraft rotational drive mechanisms

186-192

Shagov A.V., Sukhotin V.V., Zubov T.A.
Computer model of the transponder for the analysis of phase distortions of the signal

193-201

Ivanov A.V., Kushnir K.A., Simonova M.S.
Development method of splitting the radio-reflective large-sized reflector surface into cutting patterns made of mesh with coarse cells

202-210

Timofeev V.V., Trifanov I.V., Patraev E.V.
Mathematical modeling of cross-corrugated waveguide shell formation

211-219

Yatsenko M.Yu., Vorontsov V.A., Ryzhkov V.V.
System engineering research of a multirotor aircraft as a prospective technical means of exploring the atmosphere and surface of the planet Venus

220-226

Volume 6, No. 4(42), 2022

Chebotarev V.E., Fatkulin R.F., Dmitriev G.V., Lukonin N.V.
Approach of design of electric heaters used in non hermetically sealed structure spacecrafts

229-234

Chen S., Zabolotnov Yu.M.
Robust control of a hub-spoke tethered formation system of microsatellites using Hamilton-Jacobi inequality

235-245

Ivanov A.V., Kushnir K.A., Shevchugov V.O., Klimov A.N.
Development of technological equipment for autonomous testing of the shaping structure of the umbrella reflector

246-254

Gorbunov A.V., Zheltyshev O.I., Sablin A.S., Zagainov M.A., Kuznetsov S.A.
Features of the development of a simulation model of the gearbox assembly of the spacecraft drive

255-262

Udod L.S., Nagovitsin V.N.
Preparation of the surface of parts from titanium alloys for gluing with parts from polymer composite materials

263-271

Loskutov E.N., Faida Ia.V., Gubarev A.D.
Optimization and evaluation of the technical readiness of the selective laser melting for the manufacture of space technology components

272-278

Morozov N.V., Choni Yu.I., Danilov I.Yu.
Local phase center hodograph of radiating element’s navigation antenna Glonass

279-286

Gornostaev A.I.
Measures for attenuation of interference at the level of design of the measuring system of spacecraft

287-302

Volume 6, No. 3(41), 2022

Terletsky G.S., Zykov A.O., Taygin V.B.
Analysis of the designs of membrane transformable antennas for spacecraft

149-162

Sinilshchikov V.B., Kunavich S.A.
Analytical model of an arched elastomeric shock absorber for use in simulation modeling of systems

163-171

Zommer S.A., Kravchunovsky A.P.
Analysis of mechanical properties of spatial truss structures sections

172-185

Kashelkin V.V., Demidov A.S., Kapustin E.A.
Assessment of the stress state of round and annular cross-section beams made with different tensile and compressive properties materials

186-194

Kabanov А.А.
Model-based development production of rocket and space systems in the context of products in aerospace universities

195-205

Katkalov V.B., Morozova M.L.
Served space: new achievements and perspectives

206-217

Dremukhin M.A., Nagovitsin V.N.
Strategic planning of the company's development path through the development and manufacture of a ground segment of satellite communications

218-224

Volume 6, No. 2(40), 2022

Sorokin D.V., Babkina L.A., Brazgovka O.V.
Designing various-purpose subassemblies based on topological optimization

61-82

Kovalenko N.E., Vnukov A.A.
Application of electric thrusters in a spacecraft propulsion system

83-89

Girn A.V., Rudenko M.S., Taigin V.B., Mikheev A.E., Ravodina D.V.
The effect of laser surface treatment of titanium samples on the adhesive strength of adhesive joints

90-101

Mikhailov M.M., Goronchko V.A.
Optical properties and radiation stability of polypropylene modified with MgO nanoparticles

102-108

Timofeev V.V., Trifanov I.V.
Method for calculating the forces required when bending pipes of small cross-section with a rectangular profile

109-118

Popov I.P.
Electromagnetic device for spacecraft orientation

119-122

Dmitriev D.D., Tyapkin V.N., Fateev Yu.L., Gladyshev A.B., Kremez N.S.
Methods of mutual high-precision navigation based the use of relative modes of anglemeasuring receivers of global navigation satellite systems signals

123-132

Kulkov V.M., Firsyuk S.O., Yurov A.M., Tuzikov S.A., Egorov Yu.G., Yoon S.W.
Principles of construction and application areas of small spacecraft based on unified space platforms

133-143

Volume 6, No. 1(39), 2022

Yatsenko M.Yu., Vorontsov V.A.
To the question of including additional technical means in the Venus exploration program

5-13

Kravchunovsky A.P., Pryanichnikov R.A., Zommer S.A.
Program for calculating the loads generated in spacecraft structure

14-20

Dremukhin M.A., Nagovitsin V.N.
Application of additive technologies in mechanical engineering for production of form-forming riggings

21-28

Boltov E.A., Elisov N.A., Kumarin A.A., Lomaka I.A., Shafran S.V.
Design of a CubeSat thermal control system for battery module

29-37

Gladyshev A.B., Fomin A.N., Ermolenko D.S.
Mobile complex of electronic countermeasures of satellite navigation systems for unmanned aerial vehicles

38-44

Myznikova V.A., Ustimenko V.V., Chubar A.V., Solopko I.V.
Mathematical modeling of an unmanned object motion control system in SimInTech environment

45-54