Zobrazeno 1 - 5
of 5
pro vyhledávání: '"E. O. Zherebtsova"'
Publikováno v:
Proceedings of Higher Educational Institutions. Маchine Building. :99-111
The growth in the number of space debris, especially small-size debris undetectable by radars, urges the development of protective equipment for the crucial satellites and space station. Passive multilayer shields are the most effective means of prot
Publikováno v:
XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
The main aim in designing of space debris protective systems for spacecraft is providing effective shielding of the protected object with the least mass of the structure. This requires reliable data about loads acting upon the trap’s load-bearing s
Publikováno v:
XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
Creating a habitable base on Phobos is one of the most promising areas of Mars exploration. In connection with the need to create a scientific and technical foundation for the Mars development, it is relevant to analyze the possibilities of providing
Publikováno v:
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
The design of a large-sized trap for space debris is presented. The trap consists of a two-layer screen made of flexible composite materials supported by a transformable mesh frame made of a carbon fiber reinforced plastic (CFRP). The dynamics of the
Publikováno v:
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
The paper focuses on the preliminary analysis of the requirements imposed to the attitude control system of a space vehicle (SV) aimed at collecting large-size space debris (LSSD) objects. The approximate inertia matrix of Zenit-2 launch vehicle’s