A5_3 Explosive Decompression: Trajectory Troubles

Authors

  • Jamie Macquillin University of Leicester
  • John Kerr University of Leicester
  • Jack Musk University of Leicester
  • Isaac Priest University of Leicester

Abstract

In this paper we investigate and model the effects of an Explosive Decompression on the orbital trajectory of the International Space Station (ISS). We found that in an ideal, full decompression, the trajectory of the ISS would remain relatively unchanged, only affecting the altitude of perigee by 8 km.

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Published

29-11-2020

How to Cite

Macquillin, J., Kerr, J., Musk, J., & Priest, I. (2020). A5_3 Explosive Decompression: Trajectory Troubles. Physics Special Topics, 19(1). Retrieved from https://journals.le.ac.uk/index.php/pst/article/view/3694