| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8918374 | Journal of Space Safety Engineering | 2017 | 6 Pages |
Abstract
This paper will contain a critical review of the latest experimental and numerical results about the demisability of satellite propellant tanks during atmospheric re-entry from LEO.
Related Topics
Physical Sciences and Engineering
Earth and Planetary Sciences
Space and Planetary Science
Authors
T. Lips, B. Fritsche, R. Kanzler, T. Schleutker, A. Gülhan, B. Bonvoisin, T. Soares, G. Sinnema,