Analysis of use of aerodynamic systems to deorbit modular large-sized space objects from low near-earth orbits

Abstract

This paper deals with the analysis of the feasibility of aerodynamic deorbiting systems (ADS) to deorbit modular large-sized space objects (MLSO) from low earth orbit. The objective of this paper is to study the feasi-bility ADS to deorbit MLSOs from low earth orbit. The feasibility of aerodynamic deorbiting systems in the form of a single spherical shell for deorbiting modular large-sized space objects from low earth orbit is analyzed. It is shown that this is unsuitable for use. The method for deorbiting modular large-sized space objects from low earth orbits is presented. The method for deorbiting MLSOs is examined where each module is preliminarily equipped by an autonomous ADS and all modules are separated from the reference module before deorbiting. Criteria for estimation of the feasibility of ADS are selected. Studies of the feasibility of ADS for deorbiting the Mir Space Station from low earth orbit are conducted using selected criteria. The parameters of aerodynamic deorbiting systems for each module of the Mir Space Station are calculated considering the damaging effects of space on the ADS shell. The efficiency of the method proposed is estimated.

Authors and Affiliations

O. Paliy, A. Skorik

Keywords

Related Articles

Effect of modification on the formation of nonmetallic inclusions in KP-T wheel steel

This paper is concerned with the effect of the components of a multipurpose modifier on the formation of nonmetallic inclusions in KP-T wheel steel. The aim of this work is to study the effect of multipurpose modifiers o...

Special Effects of Boundary Conditions on Distribution of Elastic-Viscous- Plastic Waves into Bars Made from Delayed Fluidity Material

Based on an electromechanical model of an ideal elastic-viscous-plastic material with delayed fluidity, the propagation of elastic-viscous-plastic waves through a semi-infinite bar is considered. The problem is solved in...

Normalization of engineering system strength and reliability

This paper briefly overviews the studies conducted in 2014 – 2018 along the following research line of the Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukr...

Artificial mini-magnetosphere as a means of controlling spacecraft motion in the Earth ionosphere

Based on the results of a series of experimental studies of the interaction of spacecraft models with a hypersonic rarefied plasma flow, this paper demonstrates the possibility of controlling spacecraft motion in the ion...

Qualitative assessment of mechanical fixation of metatarsal after the chevron corrective osteotomy in Hallux Valgus

Hallux valgus is one of the most widespread diseases, which is still not clearly understood. Complications and recurrences occurring in the surgical treatment of hallux valgus call for a deeper insight into the postopera...

Download PDF file
  • EP ID EP357553
  • DOI -
  • Views 71
  • Downloads 0

How To Cite

O. Paliy, A. Skorik (2014). Analysis of use of aerodynamic systems to deorbit modular large-sized space objects from low near-earth orbits. Технічна механіка, Техническая механика, Technical Mechanics, 2(2), 43-51. https://europub.co.uk/articles/-A-357553