New Method of Engineering Evaluation of Spacecraft for Earth Remote Sensing
Journal Title: Технічна механіка, Техническая механика, Technical Mechanics - Year 2017, Vol 2, Issue 2
Abstract
The research objective is to develop a modern method of an engineering evaluation of Earth remote sensing spacecraft based on an updated hierarchy T. Saati method. Creation of methodic support for a correct engineering evaluation of the state-of-the-art technology is motivated by the importance of this factor for evaluating the competiveness of the rocket and space technology under development. The paper presents a generalized method of the engineering evaluation of rocket and space products and its specification related to the issue of an engineering evaluation of Earth remote sensing spacecraft. The method under consideration has been employed for an engineering evaluation of the Sich-2M satellite in the development of the technical project
Authors and Affiliations
V. Marchenko, Ye. Petlyak, N. Sazina, P. Khorolsky
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...
EXPERIMENTAL VERIFICATION OF A TWO-PROBE IMPLEMETRATION OF MICROWAVE INTERFEROMETRY FOR DISPLACEMENT MEASUREMENT
This paper addresses the problem of experimental verification of a recently proposed two-probe method for displacement measurement based on microwave interferometry. The aim of this paper is to develop a technique that w...
Determination of content and level of forces affecting a side frame cantilever part in operation of freight car
The paper deals with the study of additional lateral and longitudinal forces affecting the side frame cantile-ver part with its dynamic interaction with an axle box assembly of the wheel pair. The effects of additional f...
Simulation of the evolution of a droplet cloud thrown into the atmosphere as a result of an explosion of a launch vehicle with self-inflammable propellant components
The aim of this work is to develop a methodological approach to simulating the evolution of a droplet cloud (DC) formed as a result of an explosion of a launch vehicle with self-inflammable propellant components in the i...
High-speed straining sandwich elements under contact impacts
The work purpose is to analyze high-speed straining the sandwich elements at the elastoplastic stage under contact impacts. The element consisting of two thin layers from the titanium alloy and the inner ceramic layer is...