scholarly journals On the way to the optimal design of an inflatable aerodynamic decelerator of space debris removal system for CubeSat nanosatellites

Author(s):  
S V Reznik ◽  
G K Smirnov ◽  
S A Varlamov
Author(s):  
Jae-Dong Seong ◽  
Hae-Dong Kim ◽  
Ha-Yeon Choi

In a preparatory study conducted prior to the development of an active space debris removal system, a method for selecting target debris based on information such as the cumulative collision probability, the operational condition of objects, and their sizes and launch dates was developed for use in the protection of four Korea Multi-Purpose Satellite constellation satellites. This method can be used to select candidate removal targets. Two-line element data are used to identify threatening objects with high cumulative collision probability. Using information in the Satellite Catalog database, objects smaller than a certain size or objects that are currently operational were excluded from the selection range. The results of an analysis of the cumulative collision probability, object size, object type, and primary mission information showed that the COSMOS 1328, COSMOS 1862, COSMOS 375, and COSMOS 1606 satellites were suitable targets for an active debris removal mission.


Author(s):  
Shin-ichiro Nishida ◽  
Satomi Kawamoto ◽  
Yasushi Okawa ◽  
Fuyuto Terui ◽  
Shoji Kitamura

2017 ◽  
Vol 9 (2) ◽  
pp. 97-116 ◽  
Author(s):  
GUERRA Gabriele ◽  
◽  
MURESAN Alexandru Camil ◽  
NORDQVIST Karl Gustav ◽  
BRISSAUD Antoine ◽  
...  

2009 ◽  
Vol 65 (1-2) ◽  
pp. 95-102 ◽  
Author(s):  
Shin-Ichiro Nishida ◽  
Satomi Kawamoto ◽  
Yasushi Okawa ◽  
Fuyuto Terui ◽  
Shoji Kitamura

2020 ◽  
Vol 29 (1) ◽  
pp. 94-106
Author(s):  
Chongyuan Hou ◽  
Yuan Yang ◽  
Yikang Yang ◽  
Kaizhong Yang ◽  
Xiao Zhang ◽  
...  

AbstractThe increase in space debris orbiting Earth is a critical problem for future space missions. Space debris removal has thus become an area of interest, and significant research progress is being made in this field. However, the exorbitant cost of space debris removal missions is a major concern for commercial space companies. We therefore propose the debris removal using electromagnetic launcher (DREL) system, a ground-based electromagnetic launch system (railgun), for space debris removal missions. The DREL system has three components: a ground-based electromagnetic launcher (GEML), suborbital vehicle (SOV), and mass of micrometer-scale dust (MSD) particles. The average cost of removing a piece of low-earth orbit space debris using DREL was found to be approximately USD 160,000. The DREL method is thus shown to be economical; the total cost to remove more than 2,000 pieces of debris in a cluster was only approximately USD 400 million, compared to the millions of dollars required to remove just one or two pieces of debris using a conventional space debris removal mission. By using DREL, the cost of entering space is negligible, thereby enabling countries to remove their space debris in an affordable manner.


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