Email this article Preliminary design of pseudo satellites: Basic methods and feasibility criteria
- Authors: Klimenko N.N.1
-
Affiliations:
- Federal Enterprise “Lavochkin Association”
- Issue: Vol 50, No 7 (2016)
- Pages: 523-532
- Section: Article
- URL: https://journal-vniispk.ru/0038-0946/article/view/170578
- DOI: https://doi.org/10.1134/S0038094616070091
- ID: 170578
Cite item
Open Access
Access granted
Subscription Access
Abstract
Analytical models of weight and energy balances, aerodynamic models, and solar irradiance models to perform pseudo-satellite preliminary design are presented. Feasibility criteria are determined in accordance with the aim of preliminary design dependent on mission scenario and type of payload.
About the authors
N. N. Klimenko
Federal Enterprise “Lavochkin Association”
Author for correspondence.
Email: Klimenko@laspace.ru
Russian Federation, Khimki, Moscow oblast
Supplementary files
