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Volumn , Issue , 2015, Pages 1-267

Solar sails: A novel approach to interplanetary travel

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMOBILE MANUFACTURE; INTERPLANETARY FLIGHT; PROPULSION; ROCKETS; SHIP PROPULSION; SHIPS; SOLAR EQUIPMENT; SOLAR RADIATION;

EID: 84944259401     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1007/978-1-4939-0941-4     Document Type: Book
Times cited : (118)

References (177)
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    • The Minoan myth of Daedalus and Icarus is also widely available. See, for example, F. R. B. Godolphin, ed., Great Classical Myths, The Modern Library, New York, 1964.
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    • Many popular periodicals routinely review space travel progress. Two of these are the following: Spaceflight, published by the British Interplanetary Society; and Ad Astra, published by the US National Space Society. Recently, the monthly newsletter Principium of the Institute for Interstellar Studies (http://www.i4is.org/) hosts articles on deep space propulsion, spacecraft concepts and designs, and even interviews distinguished personalities among the interstellar community.
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    • Many references describe the Apollo lunar expeditions of the late 1960s and early 1970s. For example, you may consult Eric Burgess, Outpost on Apollo's Moon, Columbia University Press, NY, 1993.
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    • A more technical treatment is found in Martin J. L. Turner, Rocket and Spacecraft Propulsion, 2nd ed., Springer-Praxis, Chichester, UK, 2005. Turner's monograph also considers in greater detail many of the rocket varieties examined in this chapter.
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    • Various nuclear approaches to interstellar travel are discussed in a number of sources. For a recent popular treatment, see Paul Gilster, Centauri Dreams, Copernicus, NY, 2004.
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    • A recent technical monograph is 2nd ed., Springer-Praxis, Chichester, UK
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    • A photographic sequence showing an Orion prototype in flight is reproduced in Eugene Mallove and Gregory Matloff The Starflight Hand-book, Wiley, NY, 1989. The history of Projects Orion and Daedalus are also reviewed in this semipopular source.
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    • For a technical review of planetary gravity assist technology, interstellar ramjets, MagSails and the mini-magnetosphere, consult, 2nd ed., Springer-Praxis, Chichester, UK
    • For a technical review of planetary gravity assist technology, interstellar ramjets, MagSails and the mini-magnetosphere, consult Gregory L. Matloff Deep-Space Probes, 2nd ed., Springer-Praxis, Chichester, UK, 2005.
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    • Praxis Copernicus, Aeroassist, tethers and related technology are treated in this book as well
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    • For readers interested in science fiction stories that use the solar sail as a primary means of propulsion, we recommend ROC/Penguin, New York
    • For readers interested in science fiction stories that use the solar sail as a primary means of propulsion, we recommend Arthur C. Clarke, Project Solar Sail, ROC/Penguin, New York, 1990.
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    • For graduate students in astronautical engineering or physics, a closer presentation of sailcraft concept and the solar-wind properties can be found at Lecture 2: Sailcraft Concepts, by author Vulpetti
    • For graduate students in astronautical engineering or physics, a closer presentation of sailcraft concept and the solar-wind properties can be found at http://www.giovannivulpetti. it/SolarSailing/SailPhotonPhysics/tabid/64/Default.aspx, Lecture 2: Sailcraft Concepts, by author Vulpetti.
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    • For a more up-to-date technical treatment and review, see 2nd ed., Springer-Praxis, Chichester, UK
    • For a more up-to-date technical treatment and review, see G. L. Matloff, Deep-Space Probes, 2nd ed., Springer-Praxis, Chichester, UK, 2005.
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    • Much of the historical material in this chapter has been reviewed or referenced in 2nd ed., Springer-Praxis, Chichester, UK, A preliminary theory for the metallic perforated solar sail is also presented in that reference
    • Much of the historical material in this chapter has been reviewed or referenced in G.L. Matloff, Deep-Space Probes, 2nd ed., Springer-Praxis, Chichester, UK, (2005). A preliminary theory for the metallic perforated solar sail is also presented in that reference.
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    • Two excellent sources considering in greater depth the material covered in this chapter are Gordon and Breach
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    • More information on various sail configurations can be found in the appendix of Gregory L. Matloff Deep-Space Probes, 2nd ed., Springer-Praxis, Chichester, UK, 2005.
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    • Nanosail has been described in several sources. One useful paper is
    • Nanosail has been described in several sources. One useful paper is L. Johnson, M. Whorton, A. Heaton, R. Pinson, G. Laue, and C. Adams. "Nanosail-D: A Solar Sail Demonstration Mission," Acta Astronautica, 68, 571-575 (2011).
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    • For additional information regarding Nanosail, consult the project's website http://www. nasa.gov/mission_pages/smallsats/nanosaild.html
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    • Advances in Solar Sailing, inaugural issue, Springer
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    • (2014) Overview of IKAROS Mission
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    • The Journal of Space Technology and Science by the Japanese Rocket Society, spring
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    • (2013) Special Issue on IKAROS , vol.27 , Issue.1
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    • 17th, IFAC Symposium on Automatic Control in Aerospace, WE-P02, June 25-29, Toulouse, France. (This is the first paper showing the specific concept of Reflectance Control Device- RCD-for controlling a sailcraft in attitude. This can be considered the first reliable design concept after James Wright, who suggested the utilization of variable reflectance for space sailing in his book of 1992. The RCD has been implemented onboard IKAROS.)
    • Y. Tsuda, An Attitude Control Strategy for Spinning Solar Sail, 17th, IFAC Symposium on Automatic Control in Aerospace, WE-P02, 2007 June 25-29, Toulouse, France. (This is the first paper showing the specific concept of Reflectance Control Device- RCD-for controlling a sailcraft in attitude. This can be considered the first reliable design concept after James Wright, who suggested the utilization of variable reflectance for space sailing in his book of 1992. The RCD has been implemented onboard IKAROS.)
    • (2007) An Attitude Control Strategy for Spinning Solar Sail
    • Tsuda, Y.1
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    • Spinning solar sail orbit steering via spin rate control
    • December, (This paper explains how controlling the orbit of a spinning sail via the attitude perturbations induced by the solar radiation pressure.)
    • Y. Mimasu, T. Yamaguchi, M. Matsumoto, M. Nakamiya, R. Funase, and J. Kawaguchi, Spinning solar sail orbit steering via spin rate control, Advances in Space Research, Vol. 48, December, 2011, pp. 1810-1821 (This paper explains how controlling the orbit of a spinning sail via the attitude perturbations induced by the solar radiation pressure.)
    • (2011) Advances in Space Research , vol.48 , pp. 1810-1821
    • Mimasu, Y.1    Yamaguchi, T.2    Matsumoto, M.3    Nakamiya, M.4    Funase, R.5    Kawaguchi, J.6
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    • Generalized Attitude Model for Spinning Solar Sail Spacecraft
    • (Unique attitude behavior discovered during IKAROS operations.)
    • Y. Tsuda, T. Saiki, R. Funase, Y. Mimasu, Generalized Attitude Model for Spinning Solar Sail Spacecraft, AIAA Journal of Guidance, Control and Dynamics, Vol. 36, No. 4, 2013, pp. 967-974, doi: 10.2514/1.59516 (Unique attitude behavior discovered during IKAROS operations.)
    • (2013) AIAA Journal of Guidance, Control and Dynamics , vol.36 , Issue.4 , pp. 967-974
    • Tsuda, Y.1    Saiki, T.2    Funase, R.3    Mimasu, Y.4
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    • Achievement of IKAROS Japanese Deep Space Solar Sail Demonstration Mission
    • (This is the report of achievements after the nominal operational phase of the IKAROS mission was completed.)
    • Y. Tsuda, O. Mori, R. Funase, H. Sawada, T. Yamamoto, T. Saiki, T. Endo, K. Yonekura, H. Hoshino, J. Kawaguchi, Achievement of IKAROS Japanese Deep Space Solar Sail Demonstration Mission, Acta Astronautica, Vol. 82, No. 2, 2013, doi: 10.1016/j.actaastro. 2012.03.032 (This is the report of achievements after the nominal operational phase of the IKAROS mission was completed.)
    • (2013) Acta Astronautica , vol.82 , Issue.2
    • Tsuda, Y.1    Mori, O.2    Funase, R.3    Sawada, H.4    Yamamoto, T.5    Saiki, T.6    Endo, T.7    Yonekura, K.8    Hoshino, H.9    Kawaguchi, J.10
  • 115
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    • Development of heat sealable polyimide thin films with high space environmental stabilities for solar sail IKAROS membrane
    • Springer Berlin Heidelberg, (asymmetric thermoplastic material suitable for solar-sail petals)
    • M. Miyauchi, R. Yokota, Development of heat sealable polyimide thin films with high space environmental stabilities for solar sail IKAROS membrane, Protection of Materials and Structures from the Space Environment, Springer Berlin Heidelberg, 32, 303-316, 2012 (asymmetric thermoplastic material suitable for solar-sail petals)
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    • Miyauchi, M.1    Yokota, R.2
  • 116
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    • Novel Asymmetric Aromatic Polyimide Having Excellent Space Environmental Stability and Application for Solar Sail IKAROS Membrane
    • April (development of new polyimide chemical structures that meet some basic requirements of sail membrane working in Space)
    • R. Yokota, M. Miyauchi, Y. Ishida, Novel Asymmetric Aromatic Polyimide Having Excellent Space Environmental Stability and Application for Solar Sail IKAROS Membrane, Int. J. Soc. Mater. Eng. Resour., Vol. 20, No. 1, April 2014 (development of new polyimide chemical structures that meet some basic requirements of sail membrane working in Space)
    • (2014) Int. J. Soc. Mater. Eng. Resour. , vol.20 , Issue.1
    • Yokota, R.1    Miyauchi, M.2    Ishida, Y.3
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    • Design and development of a gossamer sail system for deorbiting in low earth orbit
    • Fernandez, Juan M., et al. "Design and development of a gossamer sail system for deorbiting in low earth orbit." Acta Astronautica 103 (2014): 204-225
    • (2014) Acta Astronautica , vol.103 , pp. 204-225
    • Fernandez, J.M.1
  • 119
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    • A nice online review of JAXA plans for a hybrid sail/ion-drive mission to Jupiter and the Trojan asteroids can be found in presented at EPSC-DPS Joint Meeting. This is its web-address: checked successfully on May 20, 2014
    • A nice online review of JAXA plans for a hybrid sail/ion-drive mission to Jupiter and the Trojan asteroids can be found in S. Sasaki et al., Japanese mission plan for Jupiter system: the Jupiter magnetospheric orbiter and the Trojan asteroid explorer, presented at EPSC-DPS Joint Meeting 2011. This is its web-address: http://yly-mac.gps.caltech. edu/A_DPS/dps%202011%20/a_dps%202011%20program%20+%20abstracts/pdf/EPSC-DPS2011-1091. pdf, checked successfully on May 20, 2014.
    • (2011) Japanese mission plan for Jupiter system: The Jupiter magnetospheric orbiter and the Trojan asteroid explorer
    • Sasaki, S.1
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    • Many texts consider the kinematics of Hohmann transfer orbits. We used Dover, NY
    • Many texts consider the kinematics of Hohmann transfer orbits. We used R. R. Bate, D. D. Mueller and J. E. White, Fundamentals of Astrodynamics, Dover, NY (1971).
    • (1971) Fundamentals of Astrodynamics
    • Bate, R.R.1    Mueller, D.D.2    White, J.E.3
  • 121
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    • A nice source for the numerical values of astronomical and physical constants is Oxford University Press, NY
    • A nice source for the numerical values of astronomical and physical constants is K. Lodders and B. Fegley Jr., The Planetary Scientist's Companion, Oxford University Press, NY (1998).
    • (1998) The Planetary Scientist's Companion
    • Lodders, K.1    Fegley, B.2
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    • Our reference for the ion-thruster power level of the NASA Deep Space 1 probe is 2nd ed., Springer-Praxis, Chichester, UK
    • Our reference for the ion-thruster power level of the NASA Deep Space 1 probe is M. J. L. Turner, Rocket and Spacecraft Propulsion, 2nd ed., Springer-Praxis, Chichester, UK (2005).
    • (2005) Rocket and Spacecraft Propulsion
    • Turner, M.J.L.1
  • 123
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    • Deflection and Control of Gravity Tractor Spacecraft for Asteroid Deflection
    • The gravity tractor as a NEO deflection scheme has received a fair amount of attention in recent years. One reference is
    • The gravity tractor as a NEO deflection scheme has received a fair amount of attention in recent years. One reference is B. Wie, "Deflection and Control of Gravity Tractor Spacecraft for Asteroid Deflection," Journal of Guidance, Control, and Dynamics, 31, 1413-1423 (2008).
    • (2008) Journal of Guidance, Control, and Dynamics , vol.31 , pp. 1413-1423
    • Wie, B.1
  • 124
    • 84944272720 scopus 로고    scopus 로고
    • Orbit cranking by solar radiation pressure, as a method of altering orbital inclination without the expenditure of fuel, is considered by Springer-Praxis, Chichester, UK. However, this method was first considered by JPL in the 1970s
    • Orbit cranking by solar radiation pressure, as a method of altering orbital inclination without the expenditure of fuel, is considered by C. McInnes on pp. 143-146 of Solar Sailing: Technology, Dynamics, and Mission Applications, Springer-Praxis, Chichester, UK (1999). However, this method was first considered by JPL in the 1970s.
    • (1999) Solar Sailing: Technology, Dynamics, and Mission Applications , pp. 143-146
    • McInnes, C.1
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    • Paintballs may Deflect an Incoming Asteroid
    • A review of the paintball NEO-diversion suggestion is available on-line as (accessed February 14, 2013)
    • A review of the paintball NEO-diversion suggestion is available on-line as J. Chu, "Paintballs may Deflect an Incoming Asteroid," MIT News, http://web.mit.edu/newsoffice/2012/deflecting-an-asteroid-with-paintballs-1026.html (accessed February 14, 2013).
    • MIT News
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    • Deflecting Earth-Threatening Asteroids Using the Solar Collector
    • The application of the solar collector in NEO deflection is discussed in the paper
    • The application of the solar collector in NEO deflection is discussed in the paper G. L. Matloff, Deflecting Earth-Threatening Asteroids Using the Solar Collector, Acta Astronautica, 82, 209-214 (2013).
    • (2013) Acta Astronautica , vol.82 , pp. 209-214
    • Matloff, G.L.1
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    • Using both nuclear ion propulsion and solar-photon sailing for very high energy missions was first proposed and analyzed in detail by author Vulpetti in his paper paper IAA-92-0240, The World Space Congress, Aug. 28 - Sept. 5, Washington D.C
    • Using both nuclear ion propulsion and solar-photon sailing for very high energy missions was first proposed and analyzed in detail by author Vulpetti in his paper Missions to the Heliopause and Beyond by Staged Propulsion Spacecraft, paper IAA-92-0240, The World Space Congress, Aug. 28 - Sept. 5, Washington D.C. (1992)
    • (1992) Missions to the Heliopause and Beyond by Staged Propulsion Spacecraft
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    • http://climate.gsfc.nasa.gov/.
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    • http://www.pmodwrc.ch/.
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    • http://umbra.nascom.nasa.gov/sdac.html; http://sohowww.nascom.nasa.gov/.
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    • http://www.gigahertz-optik.com/database_en/html/applications-tutorials/.
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    • http://www.optics.arizona.edu/Palmer/rpfaq/rpfaq.htm.
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    • http://www.solarmonitor.org/index.php.
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    • http://www.albedoarts.net/Define.html
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    • (Ed.), Lecture Notes in Physics Series, Springer-Verlag Berlin Heidelberg, (recommended for the graduate student)
    • J. P. Rozelot (Ed.), Solar and Heliospheric Origins of Space Weather Phenomena, Lecture Notes in Physics Series, Springer-Verlag Berlin Heidelberg, 2006(recommended for the graduate student)
    • (2006) Solar and Heliospheric Origins of Space Weather Phenomena
    • Rozelot, J.P.1
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    • Effect of the total solar irradiance variations on solar-sail low eccentricity orbits
    • July/August
    • G. Vulpetti, Effect of the total solar irradiance variations on solar-sail low eccentricity orbits, Acta Astronautica, Vol. 67, No. 1-2, July/August 2010
    • (2010) Acta Astronautica , vol.67 , Issue.1-2
    • Vulpetti, G.1
  • 140
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    • Total solar irradiance fluctuation effects on sailcraft-Mars rendezvous
    • March/April
    • G. Vulpetti, Total solar irradiance fluctuation effects on sailcraft-Mars rendezvous, Acta Astronautica, Vol. 68, No. 5-6, March/April 2011
    • (2011) Acta Astronautica , vol.68 , Issue.5-6
    • Vulpetti, G.1
  • 142
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    • A new, lower value of total solar irradiance: Evidence and climate significance
    • G. Kopp and J. L. Lean, A new, lower value of total solar irradiance: Evidence and climate significance, Geophysical Research Letters, Vol. 38, L01706, doi:10.1029/2010GL045777, 2011
    • (2011) Geophysical Research Letters , vol.38
    • Kopp, G.1    Lean, J.L.2
  • 143
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    • The reader should be aware that many different authors write on Wikipedia.org independently, and in different periods. Wikipedia Staff members try to keep things simple and uniform. Nevertheless, when the technical topic is particularly complicated, these aims sacrifice many aspects of Physics and Engineering. Some numerical results regarding solar sailing reflect a particular historical period where simple physical models were assumed for the sake of simplicity. Such oversimplified models of thrust (e.g. the sail as a perfect mirror) are analytically very attractive, and hence often still nowadays used by some authors even in advanced algorithms. However, the student should be aware that any real sail is quite a different thing. Therefore, the authors of this book recommend her/him considering soon more realistic sail models in their learning exercises
    • http://en.wikipedia.org/wiki/Solar_sail. The reader should be aware that many different authors write on Wikipedia.org independently, and in different periods. Wikipedia Staff members try to keep things simple and uniform. Nevertheless, when the technical topic is particularly complicated, these aims sacrifice many aspects of Physics and Engineering. Some numerical results regarding solar sailing reflect a particular historical period where simple physical models were assumed for the sake of simplicity. Such oversimplified models of thrust (e.g. the sail as a perfect mirror) are analytically very attractive, and hence often still nowadays used by some authors even in advanced algorithms. However, the student should be aware that any real sail is quite a different thing. Therefore, the authors of this book recommend her/him considering soon more realistic sail models in their learning exercises.
  • 144
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    • (updated periodically)
    • http://www.giovannivulpetti.it/SolarSailing/SailPhotonPhysics/tabid/64/Default.aspx (updated periodically).
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    • The Aurora Project: Estimation of the Optical Sail Parameters
    • G. Vulpetti and S. Scaglione, The Aurora Project: Estimation of the Optical Sail Parameters, Special issue of Acta Astronautica, vol. 44, no. 2-4, pp. 123-132,1999.
    • (1999) Special issue of Acta Astronautica , vol.44 , Issue.2-4 , pp. 123-132
    • Vulpetti, G.1    Scaglione, S.2
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    • The measurement of transmission, absorption, emission and reflection
    • 3rd edition, McGraw-Hill, New York
    • J. M. Palmer, The measurement of transmission, absorption, emission and reflection, Handbook of Optics: Vol. II, 3rd edition, 2010, McGraw-Hill, New York
    • (2010) Handbook of Optics , vol.2
    • Palmer, J.M.1
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    • http://adsabs.harvard.edu/abs/1979Sci…205.1133E.
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    • http://archive.ncsa.uiuc.edu/Cyberia/NumRel/EinsteinTest.html.
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    • Gordon and Breach Science Publishers
    • J. L. Wright, Space Sailing, Gordon and Breach Science Publishers, 1992
    • (1992) Space Sailing
    • Wright, J.L.1
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    • The stability of inner collinear equilibrium points in the photo-gravitational elliptic restricted problem
    • V. V. Markellos, E. Perdios, K. Papadakis, The stability of inner collinear equilibrium points in the photo-gravitational elliptic restricted problem, Astrophysics and Space Science, Vol. 199, No. 1, 1993, pp. 139-146
    • (1993) Astrophysics and Space Science , vol.199 , Issue.1 , pp. 139-146
    • Markellos, V.V.1    Perdios, E.2    Papadakis, K.3
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    • rd IAF Congress, paper IAA-92-0240, at The World Space Congress, Washington D.C., (published by the American Institute of Aeronautics and Astronautics, New York)
    • rd IAF Congress, paper IAA-92-0240, at The World Space Congress, Washington D.C., 1992(published by the American Institute of Aeronautics and Astronautics, New York).
    • (1992) Missions to the Heliopause and Beyond by Staged Propulsion Spacecraft
    • Vulpetti, G.1
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    • Sailcraft at High Speed by Orbital Angular Momentum Reversal
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    • Vulpetti, G.1
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    • 3D high-speed escape heliocentric trajectories by all-metallic-sail lowmass sailcraft
    • G. Vulpetti, 3D high-speed escape heliocentric trajectories by all-metallic-sail lowmass sailcraft, Acta Astronautica 1996; 39: 161-170
    • (1996) Acta Astronautica , vol.39 , pp. 161-170
    • Vulpetti, G.1
  • 165
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    • Lectures at Dept. of Astronautical Engineering of Rome University 'La Sapienza', April-May, in /SolarSailing/SailPhotonPhysics of
    • G. Vulpetti, Fundamentals and Progress of Solar-Photon Sailing, Lectures at Dept. of Astronautical Engineering of Rome University 'La Sapienza', April-May 2013, in /SolarSailing/SailPhotonPhysics of http://www.giovannivulpetti.it
    • (2013) Fundamentals and Progress of Solar-Photon Sailing
    • Vulpetti, G.1
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    • 2nd ed., Springer-Praxis, Chichester, UK
    • G. L. Matloff, Deep-Space Probes, 2nd ed., Springer-Praxis, Chichester, UK, 2005.
    • (2005) Deep-Space Probes
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    • Studies by the International Academy of Astronautics, Key Technologies to Enable Near-Term Interstellar Scientific Precursor Missions, May 2013
    • Studies by the International Academy of Astronautics, Key Technologies to Enable Near-Term Interstellar Scientific Precursor Missions, May 2013
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    • NASA/CR-2002-211730, Chapter 4, author Vulpetti, where there is an introductory mathematical treatment of the sail degradation problem
    • NASA/CR-2002-211730, Chapter 4, author Vulpetti, where there is an introductory mathematical treatment of the sail degradation problem.
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    • Solar radiation and the beryllium hollow-body sail: 1 The ionization and disintegration effects
    • (a more comprehensive treatment of the near-Sun environmental issues.)
    • Roman Ya. Kezerashvili and Gregory L. Matloff, Solar radiation and the beryllium hollow-body sail: 1 The ionization and disintegration effects, JBIS 2007; 60:169-179 (a more comprehensive treatment of the near-Sun environmental issues.)
    • (2007) JBIS , vol.60 , pp. 169-179
    • Kezerashvili, R.Y.1    Matloff, G.L.2
  • 172
    • 84944217925 scopus 로고    scopus 로고
    • To consult the Australian on-line source with up-to-date solar wind information, key-in. The data presented in this website is refreshed at 10-minute intervals
    • To consult the Australian on-line source with up-to-date solar wind information, key-in http://www.ips.gov.au/Solar/1/4. The data presented in this website is refreshed at 10-minute intervals.
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    • Microscopic Approach to Analyze Solar-Sail Space Environment Effects
    • The analysis of the interaction between the near-Sun space environment and the beryllium hollow-body solar-photon sail required several years and resulted in many research papers. Much of this work is cited and summarized in
    • The analysis of the interaction between the near-Sun space environment and the beryllium hollow-body solar-photon sail required several years and resulted in many research papers. Much of this work is cited and summarized in Roman Ya. Kezerashvili and Gregory L. Matloff, "Microscopic Approach to Analyze Solar-Sail Space Environment Effects," Advances in Space Research, 44, 859-869 (2009).
    • (2009) Advances in Space Research , vol.44 , pp. 859-869
    • Kezerashvili, R.Y.1    Matloff, G.L.2
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    • With regard to SI, see (SI), also published by NIST (USA)
    • With regard to SI, see The International System of Units (SI), also published by NIST (USA), http://www.nist.gov/index.html
    • The International System of Units
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    • addition, a graduate student, who completed university courses in electromagnetism, may find useful analytic approach to the complicated problems of the (1) sail floating potential, and (2) degradation of the sail's reflective layer as carried out in Chap. 4 of Fast Solar Sailing, Springer, August 2012, by author Vulpetti. The effects of optical degradation of the sail's reflective layer on fast sailcraft trajectories are dealt with in the Chap. 9 of the same book
    • In addition, a graduate student, who completed university courses in electromagnetism, may find useful analytic approach to the complicated problems of the (1) sail floating potential, and (2) degradation of the sail's reflective layer as carried out in Chap. 4 of Fast Solar Sailing, Springer, August 2012, by author Vulpetti. The effects of optical degradation of the sail's reflective layer on fast sailcraft trajectories are dealt with in the Chap. 9 of the same book.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.