[1] The NASA website. Passive de-orbit systems. [online] . Available: https://sst-soa.arc.nasa.gov/12-passive-deorbit-systems
[2] A. C. Long , D. A. Spencer , “Stability of a deployable drag devise for small satellite de-orbit” , AIAA/AAS Asterodynamics Specialist Conference, 2016
[3] B. Shumuel, “ Canadian advanced nanosatellite expermintation 7 (CanX-7) mission analysis payload design and testing “ MA Thesis of university of toronto, 2012.
[4] B. Scott cotton , “ Design, analysis, implementation and testing of the thermal cotrol and ADCS systems for the CanX-7 nanosatellite mission” MA Thesis of university of toronto, 2014.
[5] P. Harkness, M. MoRobb ,…, “ Development status of AEOLDOS-A deorbit module for small satellite, “ Advance in Space Research Journal, 2014
[6] The directory.eoportal website. Satellites missions. [online] . Available: https://directory.eoportal.org/web/eoportal/satellite-missions/n/nanosail-d2
[7] The mmadesignllc website. Dragnet de-orbit system. [online] . Available: https://mmadesignllc.com/product/dragnet-de-orbit-system/
[8] The space.skyrocket.de website. TechEDSat 3p de-orbit mechanism. [online] . Available:https://space.skyrocket.de/doc_sdat/techedsat-3.htm
[9] The digitalcommons.usu.edu website. Low cost de-orbiting devse for small satellites. [online] . Available:https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3296&context=smallsat
[10] S. BALOGLU, B. ALTIN, “ Space Fan: A Mechanical De-orbiting Device System For Satellites” Aeronautics and Space Technologies Institute, Turkey.
[11] E. Blanco, “ Design of a Scalable, Adaptable and Reliable De-orbiting Mechanism” Msc in space CRANFIELD University, LULEA University Of Technology, 2017
[12] J. Andrews, K.Watry, K.Brown, “ Nanosat Deorbit and Recovery System to Enable New Missions” 25th annual AIAA/USU Conferense on Small Satellite
[13] P. Acar, M. Nikbay, A. Rustam Aslan, “ Design Optimization of a 3-Unit Satellite De-Orbiting Mechanism” conference paper, June 2012
[14] CH. Lucking, C. Colombo, C. Mclnnes, “ A Passive high altitude de-orbiting strategy” 25th annual AIAA/USU Conferense on Small Satellite
[15] T. Mogi, T. Kuwahara, H. Uto, “ Structural Design of De-Orbit Mechanism Demonstration CubeSat FREEDOM” JSASS Aerospace Tech, Japan, 2015
[16] T. Mccrath casey sears, “ Sail, deployment and imaging technology for a nanosatellite deorbit system demonstration on CanX-7 “ MA Thesis of university of toronto,2014.
[17] M. Buscher, W. Chang chonge, et.c “ cubesat standards Handbook” janaury , 2017
[18] O. Boisard, “Solar Sails,” [Online Document] Jul. 2007, [2010 Aug], Available at HTTP:
http://240plan.ovh.net/~upngmmxw/fold/pliage_a.htm
[19] A. Papa and S. Pellegrino, “Systematically Creased Thin-Film Membrane Structures,” Journal of Spacecraft and Rockets, vol. 45, no. 1, Jan.-Feb. 2008, pp. 10-18.
[20] The NorthropGrumman.com website. Stem booms. [online] . Available:
https://www.northropgrumman.com /BusinessVentures/AstroAerospace/Products/Pages/STEM.aspx
[21] The globalspec.com website. Aluminized-kapton. [online] . Available: https://www.globalspec.com/industrial-directory/aluminized_kapton
[22] The alibaba.com website. Aluminum-mylar-film. [online] . Available:
https://www.alibaba.com/showroom/aluminum-mylar-film.html
[23] Hoyt, R. P., Barnes, I. M., Voronka, N. R., and Slostad, J. T., “The Terminator Tape: A Cost-Effective De-Orbit Module for End-of-Life Disposal ofLEOSatellites,” AIAA Space 2009 Conference, AIAA Paper 2009-6733, 2009.
[24] Forward, R. L., Hoyt, R. P., and Uphoff, C.W., “Terminator TetherTM: A Spacecraft Deorbit Device,” Journal of Spacecraft and Rockets, Vol. 37, No. 2, 2000, pp. 187–196. doi:10.2514/2.3565
[25] Maessen, D. C., van Breukelen, E. D., Zandbergen, B. T. C., and Bergsma, O. K., “Development of a Generic Inflatable De-Orbit Device for CubeSats,” Proceedings of the 58th International Astronautical Congress, ResearchGate, Berlin, 2007.
[26] Viquerat, A., Schenk, M., Sanders, B., and Lappas, V. J., “Inflatable Rigidisable Mast for End-of-Life Deorbiting System,” European Conference on Spacecraft Structures, Materials and Environmental Testing (SSMET), Univ. of Bristol, Bristol, U.K., April 2014.
[27] L. Visagie, "Gossamer Sails for Satellite De-orbiting: Mission Analysis and Applications" Doctoral dissertation, university of surrey, 2015
[28] A. C. Long, " DEVELOPMENT OF A PASSIVELY STABLE PYRAMID SAIL TO DEORBIT SMALL SATELLITES", Doctoral dissertation, Georgia Institute of Technology, 2018
[29] U.S. Standard Atmosphere, 1976 (National Aeronatics and Space Administration) 241 p MF A01; SOD $6.20, N77-16482.
[30] S. Trofimov, M. Ovchinnikov, “Performance Scalability of Square Solar Sails", Spacecraft and Rockets Journal, 2017.