From the First Manned Mission into Space to the Permanently Manned Orbital Station

2021 ◽  
Author(s):  
M.Yu. Belyaev ◽  
G.P. Anshakov
Keyword(s):  
Orbital Station

On measurements of low-frequency microaccelerations onboard orbital station Mir with the use of thermal convection sensor DACON

2000 ◽  
Author(s):  
V. Sazonov ◽  
G. Putin ◽  
I. Babushkin ◽  
G. Bogatyrev ◽  
A. Glukhov ◽  
...  
Keyword(s):  
Thermal Convection ◽  
Low Frequency ◽  
Orbital Station

Scientific and engineering problems involved in the implementation of the project «Manned space systems and complexes»

2019 ◽  
pp. 5-19
Author(s):  
Yevgeny A. Mikrin
Keyword(s):  
Program Completion ◽  
Search And Rescue ◽  
Current Status ◽  
Space Systems ◽  
Power Module ◽  
Orbital Station ◽  
Launch Site ◽  
New Instrumentation ◽  
Manned Space ◽  
Manned Spaceflight

This paper, which is, to a large extent, a review, presents results of an analysis of the current status and future prospects for the development of our country’s manned spaceflight from the standpoint of RSC Energia as the prime organization in Russia in this field of science and engineering. It addresses the issues involved in the ISS Russian Segment deployment completion, which is to be achieved by the addition of three new modules currently being developed at RSC Energia: the Multipurpose Laboratory Module in 2020; the Node Module in 2021; Science and Power Module in 2022, and the development of an improved version of cargo spacecraft Progress-MS. It describes quick ISS rendezvous profiles for crew and cargo transportation spacecraft. It discusses the issues involved in improving the efficiency of the ISS Russian Segment utilization, commercialization problems and plans to expand scientific applied research. The paper explores the desirability of establishing a Russian orbital station after the ISS program completion. As a strategic outlook for the development of our country’s manned space flight the paper formulates proposals on the national program of lunar research and exploration. It summarizes RSC Energia’s proposals on the development of a multifunctional system for crew search and rescue during launches of manned spacecraft from Vostochny launch site. It discusses the results and problems involved in laying the scientific, engineering and manufacturing groundwork for the development of advanced manned space systems, including introduction of digital technologies, development of new instrumentation, use of composite materials, additive and robotic technologies. Key words: Manned spaceflight, ISS Russian Segment, commercialization of scientific research, Russian orbital station, lunar research and exploration program, crew search and rescue system, problems of laying the scientific and engineering groundwork.

Transfers with a rendezvous lasting no more than one orbit between close near-circular coplanar orbits

2020 ◽  
pp. 82-93
Author(s):  
Aleksandr F. BRAGAZIN ◽  
Alexey V. USKOV
Keyword(s):  
Key Words ◽  
Relative Velocity ◽  
Free Parameter ◽  
Space Station ◽  
Characteristic Velocity ◽  
Orbital Station ◽  
Orbit Transfer ◽  
Simulation Results ◽  
The Moment ◽  
Phase Differences

Consideration has been given to orbit transfers involving spacecraft rendezvous which belong to a class of coplanar non-intersecting near-circular orbits of a spacecraft and a space station. The duration of the transfer is assumed to be limited by one orbit. The feasibility of a rendezvous using an optimal two-burn orbit-to-orbit transfer is studied. To determine a single free parameter of the transfer, i.e. the time of its start, ensuring a rendezvous at a given time or at a given velocity at the end of transfer, appropriate equations have been obtained To implement in the guidance algorithms optimal three-burn correction programs are proposed to achieve a rendezvous at a given time with a specified relative velocity at the moment of spacecraft contact. A range of phase differences at the start of maneuvering is determined, within which the characteristic velocity of the rendezvous is equal to the minimum characteristic velocity of the orbit-to-orbit transfer. The paper presents simulation results for “quick" rendezvous profiles that use the proposed programs. Key words: spacecraft, orbital station, “quick” rendezvous, orbit transfer, rendezvous program.

Computer Simulation of the MIR Orbital Station Attitude Control by Means of Gyrodines

1990 ◽  
Vol 23 (8) ◽  
pp. 11-15
Author(s):  
V.A. Sarchey ◽  
V.V. Sazonov ◽  
M.Yu. Belyaev ◽  
S.G. Zykov ◽  
V.M. Stazhkov ◽  
...  
Keyword(s):  
Computer Simulation ◽  
Attitude Control ◽  
Orbital Station

BIOLOGICAL INVESTIGATIONS ON THE ORBITAL STATION “SALYUT-5”

1979 ◽  
pp. 241-246 ◽  
Author(s):  
E.N. Vaulina ◽  
L.R. Palmbakh ◽  
V.V. Antipov ◽  
I.D. Anikeeva ◽  
L.N. Kostina ◽  
...  
Keyword(s):  
Orbital Station

Measurement of background 0.1- to 2.0-MeV gamma-ray radiation onboard the orbital station MIR

1994 ◽  
Author(s):  
S. V. Krivov ◽  
Valery V. Dmitrenko ◽  
A. M. Galper ◽  
V. M. Grachev ◽  
V. I. Lyagushin ◽  
...  
Keyword(s):  
Gamma Ray ◽  
Orbital Station
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