Analysis of tape tether survival in LEO against orbital debris

Author:

Khan Shaker Bayajid,Sanmartin Juan R.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference23 articles.

1. Analysis of bare-tether systems for deorbiting LEO satellites;Ahedo;J. Spacecraft Rockets,2002

2. Cylindrical Langmuir probes beyond the orbital-motion-limited regime;Estes;Phys. Plasmas,2000

3. Flegel, S., Gelhaus, J., Wiedemann, C., Vrsmann, P., Oswald, M., Stabroth, S., Klinkrad, H., Krag, H., 2009. The MASTER-2009 space debris environment model. In: Proc. 5th European Conference on Space Debris (ESA SP-672, July 2009), Darmstadt, Germany, 30 March-2 April, 2009.

4. Forward, R.L., Hoyt, R.P., Uphoff, C., 1998. The terminator tether: a near-term commercial application of the NASA/MSFC ProSEDS experiment. In: Proceedings of the Tether Technology Interchanging Meeting, NASA CP-1998-206900, Marshall Space Flight Center, Huntsville, Alabama, USA, pp. 109.

5. Effects of high-speed impacts on CFRP plates for space applications;Francesconi;Adv. Space Res.,2012

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