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Direct Thrust Efficiency for the L’Garde Sail Surface with a Linear Reflectivity Model

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Advances in Solar Sailing

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Abstract

A measure of propulsive efficacy for the grooved L’Garde solar sail surface — the photonic thrust efficiency in the context of an equivalent smooth (i.e., not grooved) sheet — is numerically assessed for thrust in the surface normal direction, and the dependence of this metric on the illumination incidence angles (in the directions along and across the grooves) is found to have some remarkable counter-intuitive characteristics. The study is based on a simple but powerful reflectivity model which, despite being a straightforward approximation to the full optical formulation, has received little attention in the past. This model, referred to as “linear” thrust model, simplifies analysis at the cost of only a minor loss of detail shown to be insignificant in the context of other common approximations. A result of this simplification is rigorous proof that the L’Garde sail surface groove contour shapes well approximate the classic catenary curve — the hyperbolic cosine function. The insight here offered contributes both to a practical appreciation of photonic thrust models and to the better understanding of some of the thrust characteristics of the L’Garde solar sail.

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Abbreviations

A :

Parameter characterizing trough contour shape (2 + ηt/ηn)

B f , B b :

Sail sheet front and back face non-Lambertian radiation coefficients

c 1 , c 2 , … :

Integration constants

l :

Length, distance

N :

Film tension [force/length]

P, p :

Photon flow radiation pressure (P = 4.563 µ Pa at 1 AU) and thrust pressure exerted on a surface

P max :

Maximum thrust pressure on an ideally reflecting surface = 2P = 9.126 µ Pa at 1 AU

R :

Radius of curvature

r, s :

Fraction of irradiation reflected, and the fraction thereof reflected specularly

s :

Trough contour arc length, from the shape apex

t f :

Film thickness

u, v, w :

Trough contour frame of reference aligned with the direction of illumination

u(v):

Trough contour shape

0 :

Contour shape apex (illuminated in the normal direction)

n, t :

Surface normal and tangent directions

s :

Arc length along trough contour sagging film

w :

Trough width (distance between sheet support cords)

′:

“Prime:” differentiation with respect to a Cartesian variable

α :

Irradiation angular offset from the surface normal

α z :

Contour slope angle in the trough coordinate system

˙… :

“Dot:” differentiation with respect to the contour arc length s

η n , η t :

Photonic thrust coefficients in the film surface normal and tangent directions

κ :

Curvature (β = 1/R)

σ:

Film skin stress

εf, εb :

Front and back film surface emissivities

ξ, ζ:

Sail surface frame with ξ perpendicular, ζ parallel to the cords

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Correspondence to Gyula Greschik .

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Greschik, G. (2014). Direct Thrust Efficiency for the L’Garde Sail Surface with a Linear Reflectivity Model. In: Macdonald, M. (eds) Advances in Solar Sailing. Springer Praxis Books(). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-34907-2_28

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  • DOI: https://doi.org/10.1007/978-3-642-34907-2_28

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