Assess the feasibility of launch vehicles to display MEANS Taps space object from Earth orbit

Abstract

The main sources of space debris in space orbit, ways and means to minimize the near-Earth space pollution. It is shown that the main ways to combat space Muso-set is to prevent the emergence of a new and deleting already-established th. Define methods and means of O spacecraft from working orbits of the expiration of the term of active existence, the known methods and B tem of active removal of space debris larger. As wasps basic principles remove large objects from near-Earth space, is considered to manage their erection in the dense layers of the at-mosphere through the use of a special spacecraft - cosmic-ray clean sweep, which includes the propulsion system. You are a full assessment of the capabilities of carrier rockets, which can be applied to us, the withdrawal of these garbage trucks into the desired orbit.

Authors and Affiliations

Олексій Сергійович Журавель, Микола Михайлович Дронь

Keywords

Related Articles

Aerodynamic characteristics of telescopic wing

In the last decade folding tube launch of UAV became common, for which telescopic wings are reasonable. Nowadays, telescopic wing aerodynamic characteristics are researched much less than constant geometry wing. In prese...

EXPERIENCE OF COMPOSITE MATERIALS APPLICATION IN THE CONSTRUCTION OF EXPERIMENTAL TUBE LAUNCH UAV

High flight performance of the unmanned aerial vehicle (UAV) is achieved by the minimum weight airframe, powerplant, and other useful equipment and its elements. One of the effective way of minimizing the structural weig...

EFFECTIVE USE OF INDUSTRIAL HEAT PUMP INSTALLATIONS MOLDING WORKSHOP OF THE ENTERPRISE «SEA SPECIALIZED PORT " NIKA- TERA " NIKOLAEV

To date, the development of equipment of air conditioning, ventilation and heating systems, and their efficiency and economy become more urgent. As this issue of energy resources on the world market is very serious, almo...

Stress-deformed state of composite shells with filler

This paper presents a methodology for calculating of composite layered shells with a rigid filler, which is based on the variational-grid approach for the formation of the required functionals with subsequent minimizatio...

The estimated available center of gravity range aircraft with joined wing configuration

Aircraft is a persistent overload if it independently, without pilot intervention to retain original overload flight mode and return to it after the termination of indignation. Using panel-vortex method of symmetrical f...

Download PDF file
  • EP ID EP543340
  • DOI -
  • Views 68
  • Downloads 0

How To Cite

Олексій Сергійович Журавель, Микола Михайлович Дронь (2015). Assess the feasibility of launch vehicles to display MEANS Taps space object from Earth orbit. Інформаційні системи, механіка та керування, 0(12), 99-111. https://europub.co.uk/articles/-A-543340