Flight module and Venus entry vehicle

Authors: Dugin D.A.
Published in issue: #8(13)/2017
DOI: 10.18698/2541-8009-2017-8-154
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture
Keywords: spacecraft, flight module, reentry vehicle, aerodynamic characteristics, transmitting antenna, pressurized compartment
Published: 12.07.2017

We developed a spacecraft consisting of a flight module and a reentry vehicle. The flight module serves to provide the spacecraft attitude control throughout the Earth-Venus flight. It also ensures the conditions necessary for the normal operation of the spacecraft. In the reentry vehicle there is a pressurized compartment for placing the research equipment there, as well as a central pressurized instrument compartment and a compartment for placing payloads.

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