Selection and Justification of Rational Design Solutions when Developing a Long‑Length Spatial Structure of the Solar Exploration Spacecraft

Aeronautical and Space-Rocket Engineering


Аuthors

Plaskeev N. A.1*, Kudryavtsev A. A.2**

1. Lavochkin Research and Production Association, NPO Lavochkin, , Khimki, Moscow region, Russia
2. Federal State Scientific Agroengineering Center All-Russian Institute for Mechanization, Moscow, Russia

*e-mail: plaskeevna@laspace.ru
**e-mail: kudralex94@yandex.ru

Keywords:

long‑length spatial structure, solar exploration spacecraft, dynamic parametric characteristics, photovoltaic solar panel, liquid‑propellant rocket propulsion system with high‑ and low‑thrust engines, electrojet propulsion system

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