Work

Research on reliability of pulsed electrothermal propulsion system of nanosatellite

Year: 2021

Type: article

Abstract: In the paper have been discussed nanosetellite propulsion system normalization actual themes, as well their acknowledgement by the testing results. To secure needed survival probability P≥0,995, the propulsion system bottlenecks normalized values are defined. The results of propulsion system fatigue test and reliability evaluation also have been presented. The realized count of propulsion system pulse mode switching is 15700. The actual value testing propulsion system survival probability is P=0,9979. That confirms the ability of nanosatellite propulsion system demanded reliability.

Source: Omsk Scientific Bulletin Series Aviation-Rocket and Power Engineering

DOI: 10.25206/2588-0373-2021-5-4-75-82

Authors: V. N. Blinov, V. V. Kositsin, A. I. Lukyanchik, P. V. Stepen, P. S. Yachmenev

Institution: Omsk State Technical University

Language: English

Topic: Spacecraft Design and Technology

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: diamond

OpenAlex ID: W4205346223

FWCI: 0.127

Cites: 12

Cited by: 1

Related to: 10