TY  - JOUR
T1  - Advancement of Design Technologies for Small Remote Earth’s Sensing Satellites
AU - L. Safronov, Sergey AU - Volgin, Sergey S. AU - A. Ivanushkin, Maksim 
JO  - Journal of Engineering and Applied Sciences
VL  - 14
IS  - 9
SP  - 2853
EP  - 2857
PY  - 2019
DA  - 2001/08/19
SN  - 1816-949x
DO  - jeasci.2019.2853.2857
UR  - https://makhillpublications.co/view-article.php?doi=jeasci.2019.2853.2857
KW  - complexing
KW  -construction integration
KW  -design
KW  -remote sensing of the Earth
KW  -Small satellite
KW  -method
KW  -reliability
AB  - One of the key goals of satellite design is reduction of system’s mass while maintaining high
reliability (probability of faultless operation). Every technological decision made is based on the goal of the
project, available production and technological base, material and time resourses and designer’s experience.
A large number of iterations of design work at enterprises could be often attributed to the established features
(traditions) of the organization of work of designers and technologists. There is a demand for advancement of
satellite design methods. Development of every satellite component should be carried out within a set of shared
models of structural loading, thermal conditions assembly model, unified functional model and a unified model
for the formulation and execution of design requirements. This approach to design is theoretically justified.
Also, this approach is published in a more systematic way and is compared with other approaches.
ER  -