Comparative Study of Planetary Atmospheres and Implications for Atmospheric Entry Missions
Athul Pradeepkumar Girija

TL;DR
This paper compares planetary atmospheres to evaluate the challenges and engineering considerations for atmospheric entry and aerocapture missions across different planets in the Solar System.
Contribution
It provides a comprehensive comparison of planetary atmospheres and discusses their implications for designing entry and aerocapture systems for future missions.
Findings
Venus has a thick atmosphere causing high deceleration and heating.
Mars has a thin atmosphere allowing low heating but insufficient for soft landing.
Jupiter and Saturn have high entry speeds and heating, making them highly demanding for entry and impractical for aerocapture.
Abstract
The study of planetary atmospheres is critical to our understanding of the origin and evolution of the Solar System. The combined effect of various physical and chemical processes over billions of years have resulted in a variety of planetary atmospheres across the Solar System. This paper performs a comparative study of planetary atmospheres and their engineering implications for future entry and aerocapture missions. The thick Venusian atmosphere results in high deceleration and heating rates and presents a demanding environment for both atmospheric entry and aerocapture. The thin Martian atmosphere allows low aerodynamic heating, but itself is not enough to decelerate a lander to sufficiently low speeds for a soft landing. With their enormous gravity wells, Jupiter and Saturn entry result in very high entry speeds, deceleration, and heating making them the most demanding destinations…
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Taxonomy
TopicsAstro and Planetary Science · Spacecraft Dynamics and Control · Space Satellite Systems and Control
