[1] J. H. Han and C. G. Kim, "Low earth orbit space environment simulation and its effects on graphite/epoxy composites,"
Composite structures, vol. 72, no. 2, pp. 218-226, 2006,
https://doi.org/10.1016/j.compstruct.2004.11.007.
[2] M. Tagawa and K. Yokota, "Atomic oxygen-induced polymer degradation phenomena in simulated LEO space environments: How do polymers react in a complicated space environment?,"
Acta Astronautica, vol. 62, no. 2-3, pp. 203-211, 2008,
https://doi.org/10.1016/j.actaastro.2006.12.043.
[3] E. M. Silverman, "Space environmental effects on spacecraft: LEO materials selection guide," NASA, Rep. NASA-CR-4661-PT-1, 1995.
[4] P. Gordo, T. Frederico, R. Melicio, S. Duzellier, and A. Amorim, "System for space materials evaluation in LEO environment,"
Advances in Space Research, vol. 66, no. 2, pp. 307-320, 2020,
https://doi.org/10.1016/j.asr.2020.03.024.
[5] S. Mercer, "Cryogenics: A technological tool for space scientists,"
Cryogenics, vol. 8, no. 2, pp. 68-78, 1968,
https://doi.org/10.1016/0011-2275(68)90044-1
[6] G. Maral, M. Bousquet, and Z. Sun, Satellite communications systems: Systems, techniques and technology, 6th ed., John Wiley, 2020.
[7] M. M. Finckenor and K. de Groh, A, Researcher’s Guide to: Space Environmental Effects, the NASA ISS Research Integration Office, 2015
[8] Y. Liu, P. Shi, X. Zhang, J. Lei, and W. Ding, "Laboratory plasma devices for space physics investigation,"
Review of Scientific Instruments, vol. 92, no. 7, 2021, Art. no. 071101,
https://doi.org/10.1063/5.0021355.
[9] H. Mirzaei, M. Kazemi, G. Etaati, M. Abbasi, M. Karimi, and H. Rajabalinia Jelodar Kafshgari, "Analysis and design of microwave resonant plasma source for Iranian Space Plasma Simulation Chamber,"
Journal of Theoretical and Applied Physics, vol 16, no. 3, pp. 1-6, 2022,
https://oiccpress.com/jtap/article/view/1926.
[10] C. T. G. Smith, M. Delkowki, J. V. Anguita, D. C. Cox, C. Haas, and S. R. P. Silva, "Complete atomic oxygen and uv protection for polymer and composite materials in a low earth orbit,"
ACS Applied Materials and Interfaces, vol. 13, no. 5, pp. 6670-6677, 2021,
https://doi.org/10.1021/acsami.0c21552.
[11] J. W. Chamberlain and D. M. Hunten, Theory of Planetary Atmospheres: An Introduction to Their Physics and Chemistry, 2nd ed., Academic Press, 1990.
[12] R. L. Kiefer and R. A. Orwoll, "Space environmental effects on polymeric materials," NASA,Tech. Rep. NAS 1.26:182454
[13] G. Liu, L. Cheng, X. Luan, and J. Zhang, "Damage behavior of atomic oxygen on CVD SiC coating-modified carbon/carbon composite in low earth orbit environment,"
Journal of Materials Science and Technology, vol. 35, no. 12, pp. 2957-2965, 2019,
https://doi.org/10.1016/j.jmst.2019.08.011.
[14] J. Dever, B. Banks, K. de Groh, and S. Miller, "Degradation of spacecraft materials," in
Handbook of Environmental degradation of materials, Edited by M. Kutz, Elsevier, 2005, pp. 465-501,
https://doi.org/10.1016/B978-081551500-5.50025-2.
[15] J. A. Townsend, P. A. Hansen, M. W. McClendon, K. K. De Groh, B. A. Banks, and J. Triolo, "Ground-based testing of replacement thermal control materials for the Hubble Space Telescope,"
High Performance Polymers, vol. 11, no. 1, pp. 63-80, 1999,
https://doi.org/10.1088/0954-0083/11/1/006.
[17] C. Soares and R. Mikatarian, "Understanding and control of external contamination on the international space station," in 9th International Symposium on Materials in a Space Environment, Noordwijk, Netherlands, 2003, Paper ESA SP-540.
[18] H. G. Pippin, E. Normand, S. L. Wolf, and R. Kamenetzky, "Analysis of metallized TeflonTM thin-film materials performance on satellites,"
Journal of Spacecraft and Rockets, vol. 41, no. 3, pp. 322-325, 2004,
https://doi.org/10.2514/1.10725.
[19] B. A. Banks, K. K. de Groh, and S. K. Miller, "Low earth orbital atomic oxygen interactions with spacecraft materials,"
2- MRS Online Proceedings Library, Volume 851: Symposium NN – Materials for Space Applications, 2004, Art. no. NN8.1, https://doi.org/10.1557/PROC-851-NN8.1.
[20] D. H. Hathaway, "Solar cycle prediction," (1999) NASA, MSFC.[Online]. Available:
http://solarscience.msfc.nasa.gov/predict.shtml, 1999
[21] A. H. Stambler, K. E. Inoshita, L. M. Roberts, C. E. Barbagallo, K. K. de Groh, and B. A. Banks, "Ground laboratory to in‐space atomic oxygen correlation for the peace polymers," in
AIP conference proceedings, American Institute of Physics, 2009, vol. 1087, no. 1, pp. 51-66,
https://doi.org/10.1063/1.3076865.
[22] G. Liu, C. Laifei, L. Xingang, and Z. Jiaxin. "Damage behavior of atomic oxygen on CVD SiC coating-modified carbon/carbon composite in low earth orbit environment,"
Journal of Materials Science and Technology, vol 35, no. 12, pp. 2957-2965, 2019,
https://doi.org/10.1016/j.jmst.2019.08.011.
[23] W. M. Mahmoud, D. Elfiky, S. M. Robaa, M. S. Elnawawy, and S. M. Yousef. "Effect of atomic oxygen on LEO CubeSat,"
International Journal of Aeronautical and Space Sciences, vol. 22, pp. 726-733 2021,
https://doi.org/10.1007/s42405-020-00336-w.
[24] J. Dever, B. Banks, K. de Groh, and S. Miller, "Degradation of spacecraft materials," in
Handbook of environmental degradation of materials: Elsevier, 2005, pp. 465-501,
https://doi.org/10.1016/B978-081551500-5.50025-2.
[25] D. Shoots, "Update on 3 major debris clouds,"
Orbital Debris Quarterly, vol. 14, no. 2, pp. 1-3, 2010,
https://orbitaldebris.jsc.nasa.gov/.
[26] B. Berger, "Battery likely caused explosion aboard military weather sat," (2015, Mar. 3). [Online]. Available:
http://spacenews.com/battery-likely-the-culprit-in-military-weather-satellite-explosion
[27] P. Anz-Meador, "Orbital debris quarterly news."
Orbital Debris Quarterly News (ODQN), vol. 24, no. 1, 2020,
https://orbitaldebris.jsc.nasa.gov/.
[28] NASA ODPO (National Aeronautics and Space Administration Orbital Debris Program Office). Spatial density distributions of the tracked objects in low Earth orbit (LEO) for 1 January 2007 and 1 January 2014. National Aeronautics and Space Administration Orbital Debris Quarterly News, vol. 18, no. 2, 2015,
https://orbitaldebris.jsc.nasa.gov/.
[29] NASA ODPO (National Aeronautics and Space Administration Orbital Debris Program Office). 2015a. Monthly effective mass of objects in Earth orbit by region. National Aeronautics and Space Administration Orbital Debris Quarterly News, vol. 19, no. 1, 2015,
https://orbitaldebris.jsc.nasa.gov/.
[30] NASA ODPO (National Aeronautics and Space Administration Orbital Debris Program Office). 2015b. International Space Station performs fourth and fifth debris avoidance maneuvers of 2014. National Aeronautics and Space Administration Orbital Debris Quarterly News vol. 19, no. 1, 2015,
https://orbitaldebris.jsc.nasa.gov/.
[31] J. H. Han and C. G. Kim,"Low earth orbit space environment simulation and its effects on graphite/epoxy composites,"
Composite structures, vol. 72, no. 2, pp. 218-226, 2006,
https://doi.org/10.1016/j.compstruct.2004.11.007.
[32] R. S. Soler Chisabas, E. Escobar Burger, and G. Loureiro, "Space simulation chambers state-of-the-art," in 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 2016, pp. 26-30.
[33] S. O. Park, J. B. Moon, Y. G. Lee, C. G. Kim, and S. Bhowmik. "Usage of fiber Bragg grating sensors in low earth orbit environment," in
Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems, Spie Smart Structures and Materials + Nondestructive Evaluation And Health Monitoring, San Diego, California, United States, vol. 6932, 2008, pp. 526-533,
https://doi.org/10.1117/12.776631.
[34] R. vargas bernal, "Advances in electromagnetic environmental shielding for aeronautics and space applications," in
Recent Trends on Electromagnetic Environmental Effects for Aeronautics and Space Applications, edited by Christos D. Nikolopoulos
, IGI Global, 2021, pp. 80-96,
https://doi.org/10.4018/978-1-7998-4879-0.ch003.
[35] P. Gordo, T. Frederico, R. Melicio, S. Duzellier, and A. Amorim,"System for space materials evaluation in LEO environment,"
Advances in Space Research, vol. 66, no. 2, 2020, pp. 307-320,
https://doi.org/10.1016/j.asr.2020.03.024.
[36] T. D. S. Frederico, "Development of a cryogenic facility for the generation of space debris," M.S. Thesis, Faculdade de Cieˆncias, Universidade de Lisboa, Portugal, France 2017.
[37] H. N. Yeritsyan
et al.," Space low earth orbit environment simulator for ground testing materials and devices,"
Acta Astronautica, vol. 181, 2021, pp. 594-601,
https://doi.org/10.1016/j.actaastro.2021.01.030.
[38] J. Kleiman, S. Horodetsky, V. Sergeyev, V. Issoupov, and R. Ng. "Critical review of the design of space environment simulators: lessons learnt." in the 10th international symposium on materials in a space environment, Collioure, France, 2006.
[39] K. Wilson, , R. C. Álvaro, M. Bengtson, J. Hammerl, J. Maxwell, and H. Schaub, "Development and characterization of the ECLIPS space environments simulation facility,"
Acta Astronautica, vol. 194, 2022, pp. 48-58,
https://doi.org/10.1016/j.actaastro.2021.12.037.
[40] K. Wilson, M. Bengtson, Á. Romero-Calvo, J. Maxwell, and H. Schaub, "Characterization of the ECLIPS space environments simulation facility," in AIAA Scitech 2021 Forum, Virtual Event, 2021, Paper 1538.
[41] H. Alisadesghi, H. Ramezani-Najafi, and H. R. Abbas," Design and construction of the thermal model and thermal balance test of atest satellite," Journal of Space Science and Technology, vol. 9, no. 2, pp. 61-76, 2016, (in Persion).
[42] "
Vacuum Test and Thermal Cycle," (2023, May. 1), (in Persian). [Online]. Available:
https://www.lab.isrc.ac.ir.
[43] "
Aerospace Research Institute, Temperature Chamber Device," (2019, Jan. 29), (in Persian). [Online]. Available:
https://www.ari.ac.ir/index.php/fa/2019-01-29-06-35-49.
[44] H. Zinivand, "The Thermal Vacuum Test of the "Pars 1" Propulsion System was Successfully Completed," (2023, May. 1), (in Persian). [Online]. Available:
https://www.iranhavafaza.com/index/article/2306.
[45] "
Atmospheric Test Chamber - Vacuum Chamber,"
(2022, Jan. 22), (in Persian). [Online]. Available:
Products - aryasarmayesh.