Journal "Vestnik "NPO IM. S.A.Lavochkina"
Contents of the issue
Editorial articlePichkhadze K.M., Finchenko V.S., Aleksashkin S.N., Ostreshko B.A.
The transformable descent modules
Kuzin Е.N., Zagarskih V.I., Efanov V.V.
Solution of task of the shock wave attenuation in an obstacle during contact explosion of high-energy material charge
Evgrafov A.E., Pol V.G.
Geometry of the Earth sounding by space radar using synthetic aperture technology and geolocation of the acquired images
Golomazov M.M., Ivankov A.A.
Computational and theoretical study of the impact of the Mars atmosphere on the «ExoMars-2018» descent module during aerodynamic braking
Kotomin А.А., Harchenko V.V., Dushenok S.A., Vasilev A.V., Efanov V.V., Gorovtsov V.V.
Analytical and experimental studies of strength and reliability of indestructible detonation translators of spacecraft separation systems
Shirshakov A.E., Novichkov V.M., Savkin L.V., Makarov A.S.
Enhancement of the functional capabilities of control and diagnostic system for SC onboard control system due to built-in reconfigurable computing structures
Matushin M.M., Mishurova N.V., Skobelev P.O., Laruhin V.B.
Intelligent technologies for decision support during parrying emergency situations on international space station (completion)
Barabanov А.А., Vyatlev P.А., Larchenko Yu.V., Sergeev D.V., Stekolshchikov O.Yu., Suborev K.G., Sysoev V.К.
Laser perforation of film polymeric materials for spacecraft's multi-layer insulation
Ivanyukhin A.V., Petukhov V.G.
Optimization of spacecraft with minimum power solar electric propulsion system interplanetary trajectories
Konstantinov M.S., Nguyen D.N.
Analysis of ballistic capabilities for rejection of disturbances connected with temporary contingency cutoff of the electric propulsion
Sentsov Ju.I., Hmelshchikov M.V.
The dependence between the weight of the Earth remote sensing spacecraft and the spatial resolution of imaging equipment
Ivanov N.N., Ivanov A.N.
On-board module for extraterrestrial particles capture and its return to the Earth
Mozgovoy Y.V.
The concepts used to develop hardware and software for control unit of electrical devices of automatic autonomic long-living spacecraft