TY - CHAP
T1 - Potential effects of optical solar sail degredation on trajectory design
AU - Dachwald, Bernd
AU - Baturkin, Volodymyr
AU - Coverstone, Victoria L.
AU - Diedrich, Benjamin
AU - Garbe, Gregory P.
AU - Gorlich, Marianne
AU - Leipold, Manfred
AU - Lura, Franz
AU - Macdonald, Malcolm
AU - McInnes, Colin R.
AU - Mengali, Giovanni
AU - Quarta, Alessandro A.
AU - Rios-Reyes, Leonel
AU - Scheeres, Daniel J.
AU - Sebolt, Wolfgang
AU - Wie, Bong
PY - 2005
Y1 - 2005
N2 - The optical properties of the thin metalized polymer films that are projected for solar sails are assumed to be affected by the erosive effects of the space environment. Their degradation behavior in the real space environment, however, is to a considerable degree indefinite, because initial ground test results are controversial and relevant inspace tests have not been made so far. The standard optical solar sail models that are currently used for trajectory design do not take optical degradation into account, hence its potential effects on trajectory design have not been investigated so far. Nevertheless, optical degradation is important for high-fidelity solar sail mission design, because it decreases both the magnitude of the solar radiation pressure force acting on the
sail and also the sail control authority. Therefore, we propose a simple parametric optical solar sail degradation model that describes the variation of the sail film's optical coefficients with time, depending on the sail film's environmental history, i.e., the radiation dose. The primary intention of our model is not to describe the exact behavior
of specific film-coating combinations in the real space environment, but to provide a more general parametric framework for describing the general optical degradation
behavior of solar sails. Using our model, the effects of different optical degradation behaviors on trajectory design are investigated for various exemplary missions.
AB - The optical properties of the thin metalized polymer films that are projected for solar sails are assumed to be affected by the erosive effects of the space environment. Their degradation behavior in the real space environment, however, is to a considerable degree indefinite, because initial ground test results are controversial and relevant inspace tests have not been made so far. The standard optical solar sail models that are currently used for trajectory design do not take optical degradation into account, hence its potential effects on trajectory design have not been investigated so far. Nevertheless, optical degradation is important for high-fidelity solar sail mission design, because it decreases both the magnitude of the solar radiation pressure force acting on the
sail and also the sail control authority. Therefore, we propose a simple parametric optical solar sail degradation model that describes the variation of the sail film's optical coefficients with time, depending on the sail film's environmental history, i.e., the radiation dose. The primary intention of our model is not to describe the exact behavior
of specific film-coating combinations in the real space environment, but to provide a more general parametric framework for describing the general optical degradation
behavior of solar sails. Using our model, the effects of different optical degradation behaviors on trajectory design are investigated for various exemplary missions.
KW - solar sails
KW - guidance systems
KW - space travel
KW - spacecraft
KW - trajectory design
UR - http://www.space-flight.org/AAS_meetings/2005_astro/2005_astro.html
M3 - Chapter
SP - 2569
EP - 2592
BT - Proceedings of the AAS/AIAA Astrodynamics Specialist Conference
ER -