SENSOR EQUIPMENT FOR MEASUREMENT OF SPACECRAFT SPACES CHARACTERISTICS

Slavkin Ilya Evgenevich, postgraduate student, Penza State University (40 Krasnaya street, Penza, Russia),  ilya-slavkin@yandex.ru
Pronin Alexander Vladimirovich, postgraduate student, Penza State University (40 Krasnaya street, Penza, Russia), 
pronin.alexandr2017@yandex.ru

681.586+629.78

10.21685/2307-5538-2018-3-5

Background. The sensor equipment installed on space vehicles is designed to provide specified conditions inside the spacecraft and the characteristics of its movement, as well as to solve special problems associated with achieving the ultimate flight objectives. The
research objective is the development of a unified range of sensors that make up the system for recording the external impacts of space spaces.
Materials and methods. The object of the study is a system for measuring and archiving the characteristics of outer space. The subject of the study are sensor equipment, namely impact sensor, solar alarm and a powerful RF exposure sensor. In the process of work, a number of circuit-based solutions used in the design of similar products are considered, methods of mathematical modeling are applied.
Conclusions. In the development of sensor equipment, the principles for the construction of a shock sensor, the structure of a solar radiation detector, and the construction structure of a powerful radio frequency radiation sensor are proposed. The results of DA design, specific circuitry solutions, mathematical modeling are presented.

impact sensor, solar radiation detector, RF-radiation sensor