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
References
Greschik G. “Preliminary Assessment of Boom Loads for the Encounter 2001 Solar Sail Slack Design,” Consultant report to L’Garde, Inc. 15181 Woodlawn Ave, Tustin, CA 92780; February 6 2002.
Greschik G. “ROSS NRA Cycle 1 — L’Garde Solar Sail General Structural Design and Analysis,” Structural Report 2003/3, L’Garde, Inc. 15181 Woodlawn Ave, Tustin, CA 92780; November 21 2003. Revision 1 of March 25, 2003, original report.
Greschik, G., Derbes, B., Veal, G., and Rogan, J. “The Cord Mat Sail — Concept, Mechanics, And Design Example,”; AIAA 2005-2049.
Steitz DE. “Communications, Navigation And In-Space Propulsion Technologies Selected For NASA Flight Demonstration,”. Press Release 11-272. NASA Headquarters, Washington, D.C. August 22, 2011. Available at: http://www.nasa.gov/home/hqnews/2011/aug/HQ_11-272_TDM_Selections.html.
Lichodziejewski, D., Derbs, B., Sleight, D., and Mann, T. “Vacuum Deployment and Testing of a 20 m Solar Sail System,”: AIAA 2006-1705.
Greschik, G. and Mikulas, M. M. “Design Study of a Square Solar Sail Architecture,”. Journal of Spacecraft and Rockets. Vol. 39, No. 5, September–October 2002:pp. 653–661.
Derbes, B. and Lichodziejewski, D. “Propulsive Reflectivity and Photoflexibility: Effects on Solar Sail Performance and Control,”: AIAA 2006-4520.
Greschik G. “A Linear Photonic Thrust Model and its Application to the LGarde Solar Sail Surface,”: AIAA 2013-1803.
Rios-Reyes, L. and Scheeres, D. J. “Solar-Sail Navigation: Estimation of Force, Moments, and Optical Parameters,”. Journal of Spacecraft and Rockets. Vol. 30, No. 3, May-June 2007:pp. 660–668.
Greschik G. “Solar Sail Scalability and a “Truly Scalable” Architecture: the Space Tow,”. Journal of Spacecraft and Rockets. Vol. 44, No. 4, July–August 2007:pp. 831–839.
Vulpetti, G. and Scaglione, S. “The Aurora Project: Estimation of the Optical Sail Parameters,”. Acta Astronautica. Vol. 44, No. 2–4, January–February 1999:pp. 123–132.
Dachwald, B., Mengali, G., Quarta, A., and Macdonald, M. “Parametric Model and Optimal Control of Solar Sails with Optical Degradation,”. Journal of Guidance, Control, and Dynamics. Vol. 29, No. 5, September–October 2006:pp. 1170–1178.
Mengali, G., Quarta, A. A., Circi, C., and Dachwald, B. “Refined Solar Sail Force Model with Mission Application,”. Journal of Guidance, Control, and Dynamics. Vol. 30, No. 2, March–April 2007:pp. 512–520.
McInnes CR. Solar Sailing: Technology, Dynamics and Mission Applications, Springer-Praxis series in space science and technology. London, UK: Springer; 1st ed., 1999.
Wright JL. Space Sailing, Gordon and Breach Science Publishers. 1079 LH Amsterdam, the Netherlands: Overseas Publishers Association; 1st ed., 1992.
Scheeres DJ. “The Dynamical Evolution of Uniformly Rotating Asteroids Subject to YORP,”. Icarus. Vol. 188, No. 2, June 2007:pp. 430–450.
McMahon, J. W. and Scheeres, D. J. “New Solar Radiation Pressure Force Model for Navigation,”. Journal of Guidance, Control, and Dynamics. Vol. 33, No. 5, September–October 2010:pp. 1418–1428.
Quarta, A. A. and Mengali, G. “Semi-Analytical Method for the Analysis of Solar Sail Heliocentric Orbit Raising,”. Journal of Guidance, Control, and Dynamics. Vol. 35, No. 1, January–February 2012:pp. 330–335.
Rios-Reyes, L. and Scheeres, D. J. “Applications of the Generalized Model for a Solar Sail,”: AIAA 2004-5434.
Rios-Reyes, L. and Scheeres, D. J. “Generalized Model for Solar Sails,”. Journal of Spacecraft and Rockets. Vol. 42, No. 1, January-February 2005:pp. 182–185.
Woo, B., Ertmer, K. M., Coverstone, V. L., Burton, R. L., Benavides, G. F., and Carroll, D. L. “Deployment Experiment for Ultralarge Solar Sail System (UltraSail),”. Journal of Spacecraft and Rockets. Vol. 48, No. 5, September-October 2012:pp. 874–880.
Okuizumi N. “Deformations and Vibrations of a Rotating Circular Membrane under Distributed Loads,”: AIAA 2007-1803.
Atchison, J. A. and Peck, M. A. “A passive, sun-pointing, millimeter-scale solar sail,”. Acta Astronautica. Vol. 67, No. 1–2, July–August 2010:pp. 108–121.
Bolle, A. and Circi, C. “Solar sail attitude control through in-plane moving masses,”. Journal of Aerospace Engineering, Proc. IMechE: Part G. Vol. 222, No. 1, January 2008:pp. 81–94.
Circi C. “Three-axis attitude control using combined gravity-gradient and solar pressure,”. Journal of Aerospace Engineering, Proc. IMechE: Part G. Vol. 221, No. 1, January 2007:pp. 85–90.
Wie B. “Solar Sail Attitude Control and Dynamics, Part 1,”. Journal of Guidance, Control, and Dynamics. Vol. 27, No. 4, July–August 2004:pp. 526–535.
Burton, R. L., Coverstone, V. L., Hargens-Rysanek, J., Ertmer, K. M., Botter, T., Benavides, G., Woo, B., Carroll, D. L., Gierow, P. A., Farmer, G., and Cardin, J. “UltraSail - Ultra-Lightweight Solar Sail Concept,”: AIAA 2005-4117.
Ewing, A. and Moore, J. “Propulsion Sensitivity Study on NASAs Proposed ST9 Evolved Design Solar Sail using the Solar Vectoring Evaluation Tool (SVET),”: AIAA 2007-1825.
McInnes C. “Artificial Lagrange Points for a Partially Reflecting Flat Solar Sail,”. Journal of Guidance, Control, and Dynamics. Vol. 22, No. 1, January 1999:pp. 185–187.
Molostov, A. A. and Shvartsburg, A. A. “Heliocentric halos for a solar sail with absorption,”. Soviet Physics Doklady. 1992.
MacNeal RH. “The Heliogyro - An Interplanetary Flying Machine,” Tech. Rep. ARC-R-249. Santa Barbara, CA March 13 1967.
Derbes, B., Veal, G., Rogan, J., and Chafer, C. “Team Encounter Solar Sails,”: AIAA 2004-1577.
Lichodziejewski, D., Derbes, B., Slade, K., Mann, T., and Reinert, R. “Vacuum Deployment And Testing Of a 4-Quadrant Scalable Inflatable Rigidizable Solar Sail System,”: AIAA 2005-2122.
Lichodziejewski, D., Derbes, W., Reinert, R., Belvin, K., Slade, K., and Mann, T. “Development and Ground Testing of a Compactly Stowed Scalable Inflatably Deployed Solar Sail,”: AIAA 2004-1507.
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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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