Integration of controllable scientific equipment into the Russian Segment of the International Space Station

Author(s):  
Diana M. AYUKAEVA ◽  
Fedor A. VORONIN ◽  
Mikhail A. POLUARSHINOV ◽  
Mikhail A. KHARCHIKOV

The paper discusses the process of integrating scientific equipment into the Russian Segment of the International Space Station (ISS RS) to conduct space experiment using the ISS IS information and control system. The paper addresses the stages in ground processing of scientific equipment that are critical for its successful operation after delivery to the ISS RS: tests on the hardware (vibration and hydraulic tests, electromagnetic compatibility tests, incoming inspection), development of the software for the equipment using ground debugging facility and conducting integrated tests in the checkout facility. It points out the need to update the existing stages of ground preparations for experiments to reduce the hardware ground processing time. Taking as examples the space experiment Terminator and experiments conducted using cargo transportation spacecraft Progress, the paper resents results obtained through the use of the described approach. Key words: information and control system, scientific equipment, space experiment, International Space Station, logistics spacecraft Progress, microgravity.

2005 ◽  
Vol 36 (9) ◽  
pp. 1710-1717 ◽  
Author(s):  
Nevena Stojicic ◽  
David Walrafen ◽  
Christa Baumstark-Khan ◽  
Elke Rabbow ◽  
Petra Rettberg ◽  
...  

Author(s):  
Eduard N. ALEKSANDROV ◽  
Maya S. ANTIPOVA ◽  
Andrey N. KRYLOV ◽  
Aleksandr V. KASHKOVSKIY ◽  
Anna A. RODICHEVA

The goals and objectives of space experiment Control to study parameters of the induced external atmosphere of the Russian Segment of the International Space Station are presented. The processing and analysis procedure for telemetry data obtained using scientific equipment Indicator - ISS is described. Numerical calculations were performed by direct statistical modeling of the flow around the pressure sensor by incoming flotation the Earth's outer atmosphere in the background measurement conditions, as well as in disturbed conditions with two vernier engines of the Zvezda module being operated. A correction function of the pressure sensor is obtained depending on the orientation, temperature factor and selected model of interaction of incident flow molecules with the internal and external device surfaces. The results of numerical modeling of the jet discharges of the the Zvezda vernier engine were compared with the data obtained in full-scale pressure measurements in experiment Control. Key words: pressure sensor, orbital station, induced external atmosphere, direct statistical modeling method.


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