Thermite-for-demise (T4D): Experiments and numerical modelling on ball-bearing unit mock-ups containing thermite in an arc-heated wind tunnel

Autor: Finazzi, A., Daub, D., Maggi, F., Paravan, C., Dossi, S., Lips, T., Smet, G., Bodjona, K.

Publikováno v: In Acta Astronautica October 2024 223:550-576

Comparison between two spacecraft-oriented tools: PAMPERO & SCARAB

Autor: Annaloro, J. ^*, Galera, S., Kärräng, P., Prigent, G., Lips, T., Omaly, P.

Publikováno v: In The Journal of Space Safety Engineering March 2017 4(1):15-21

Demisability assessment of space materials.

Autor: Bonvoisin, B., Meisnar, M., Merrifield, J., Beck, J., Lips, T., Guelhan, A., Schleutker, T., Herdrich, G., Pagan, A., Kaschnitz, E., Liedtke, V., Helber, B., Lopes, S., Gouriet, J. B., Chazot, O., Ghidini, T.

Publikováno v: CEAS Space Journal; Jan2023, Vol. 15 Issue 1, p213-235, 23p

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TeSeR – Technology for Self-Removal – First results of an H2020 Project to develop a Post-Mission-Disposal Module

Autor: Voigt, P., Vogt, C., Schubert, R., Stokes, H., Underwood, C., Knoll, A., Ryden, K., Macdonald, M., Kerr, E., Smith, L. J., Förstner, R., Wander, A., Konstantinidis, K., Antonetti, S., Lips, T., Bisgaard, M., Anders Schmidt Kristensen, Jens Frederik Dalsgaard Nielsen, Mcinnes, C.

Publikováno v: Voigt, P, Vogt, C, Schubert, R, Stokes, H, Underwood, C, Knoll, A, Ryden, K, Macdonald, M, Kerr, E, Smith, L J, Förstner, R, Wander, A, Konstantinidis, K, Antonetti, S, Lips, T, Bisgaard, M, Kristensen, A S, Nielsen, J F D & McInnes, C 2017, ' TeSeR – Technology for Self-Removal – First results of an H2020 Project to develop a Post-Mission-Disposal Module ', Paper fremlagt ved The 7th European Conference on Space Debris, Darmstadt, Tyskland, 18/04/2017-21/04/2017 s. 1 . < https://conference.sdo.esoc.esa.int/proceedings/sdc7/paper/17/SDC7-paper17.pdf >
Aalborg University

The goal of TeSeR (Technology for Self-Removal) is to take the first step towards the development of a scalable, flexible, cost-efficient, but highly reliable Post-Mission-Disposal (PMD) module. This module is to be attached to the spacecraft (S/C) o

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::0c48dc62b2ca0d8fcefb205977359497
https://vbn.aau.dk/da/publications/2e787f23-7694-494f-afeb-aac296756ad1