Development of Space-Borne Antenna Reflector via 3D Printing

  • Jaya Kori Department of Mechanical Engineering, Indian Institute of Technology (Indian School of Mines), Dhanbad, India
  • Sampurna Patnaik Department of Mechanical Engineering, Indian Institute of Technology (Indian School of Mines), Dhanbad, India
  • Somnath Chattopadhyaya Department of Mechanical Engineering, Indian Institute of Technology (Indian School of Mines), Dhanbad, India
  • Sayan Chatternjee Department of Electronics and Telecommunications, Jadavpur University, India
  • Krishna Agarwal Department of Physics and Technology, UiT The Arctic University of Norway
Keywords: Antenna Structure, Reflector Deployability, Inflatable, Membrane, Additive Manufacturing

Abstract

The growing necessity of large aperture-based structures for many aerospace applications emphasizes the need to deploy large antenna structures in space. The space antennas should be light in weight and have low stowage volume, with efficient membrane packaging.  The concept of additive manufacturing has been introduced to reduce weight as well as cost. In this paper, a comparative study has been done to analyze the advancement made in reducing weight with adequate strength. Based on the study, the main objectives are to develop a 3D-printed spherical reflector model with high specific strength and to assess the consistency of the model's shape.  For determining the specific strength, tensile testing is performed on four different infill densities (20%, 40%, 60%, and 80%) with a grid infill pattern. It was observed that the specimen with 80% infill density has the highest tensile strength, 36.56 MPa, which is 23.51% more than 20% infill. However, the specimen with 20% infill density has the highest specific strength of 19.323 GPa/kg among the four specimens, which is approximately 64.64% higher than the 100% infill density. As a result of the testing, the spherical reflector model is 3D printed with 20% infill density, and it was found that the model achieves its shape stability and shape consistency with adequate specific strength.

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References

Abdullah, H. H., Elboushi, A., Gohar, A. E., & Abdallah, E. A. (2021). An Improved S-Band CubeSat Communication Subsystem Design and Implementation. IEEE Access, 9, 45123–45136. https://doi.org/10.1109/ACCESS.2021.3066464

Baars, J. W. M. (2003). Characteristics of a reflector antenna. ESO NRAO Electronic, Tucson, Internal Report ALMA Memo, 456.

Babuscia, A., Choi, T., Sauder, J., Chandra, A., & Thangavelautham, J. (2016). Inflatable antenna for CubeSats: Development of the X-band prototype. IEEE Aerospace Conference Proceedings, 2016-June. https://doi.org/10.1109/AERO.2016.7500679

Babuscia, A., Sauder, J., Chandra, A., Thangavelautham, J., Feruglio, L., & Bienert, N. (2017, June 7). Inflatable antenna for cubesat: A new spherical design for increased X-band gain. IEEE Aerospace Conference Proceedings. https://doi.org/10.1109/AERO.2017.7943897

Balaji, D., Ranga, J., Bhuvaneswari, V., Arulmurugan, B., Rajeshkumar, L., Manimohan, M. P., Devi, G. R., Ramya, G., & Masi, C. (2022). Additive Manufacturing for Aerospace from Inception to Certification. Journal of Nanomaterials, 2022, https://doi.org/10.1155/2022/7226852

Blakey-Milner, B., Gradl, P., Snedden, G., Brooks, M., Pitot, J., Lopez, E., Leary, M., Berto, F., & du Plessis, A. (2021). Metal additive manufacturing in aerospace: A review. Materials and Design, 209. https://doi.org/10.1016/j.matdes.2021.110008

Bouzidi, R., & Lecieux, Y. (2012). A numerical method to optimize the design of a space inflatable membrane reflector. Acta Astronautica, 74, 69–78. https://doi.org/10.1016/j.actaastro.2011.12.009

Cai, J., Deng, X., Xu, Y., & Feng, J. (2016). Motion analysis of a foldable barrel vault based on regular and irregular Yoshimura origami. Journal of Mechanisms and Robotics, 8(2), 021017. https://doi.org/10.1115/1.4031658

Chahat, N., Hodges, R. E., Sauder, J., Thomson, M., Peral, E., & Rahmat-Samii, Y. (2016). CubeSat Deployable Ka-Band Mesh Reflector Antenna Development for Earth Science Missions. IEEE Transactions on Antennas and Propagation, 64(6), 2083–2093. https://doi.org/10.1109/TAP.2016.2546306

Chandra, A., Carlos, J., Tonazzi, L., Stetson, D., Pat, T., Walker, C. K., & Observatory, S. (2020). Inflatable membrane antennas for small satellites; Inflatable membrane antennas for small satellites. In 2020 IEEE Aerospace Conference.

Derise, M. R., Rahmat Derise, M., & Zulkharnain, A. (2021). Effect of Infill Pattern and Density on Tensile Properties of 3D Printed Polylactic acid Parts via Fused Deposition Modeling (FDM). In Article in International Journal of Mechanical & Mechatronics Engineering. https://www.researchgate.net/publication/353764104

Fang, H., Shook, L., Lin, J. K. H., Pearson, J. C., & Moore, J. D. (2012). A large and high radio frequency deployable reflector. 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012. https://doi.org/10.2514/6.2012-1838

Gossamer Spacecraft: Membrane And Inflatable Structures Technology For Space Applications. (2001). In Gossamer Spacecraft: Membrane And Inflatable Structures Technology For Space Applications. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/4.866616

Helena, D., Ramos, A., Varum, T., & Matos, J. N. (2020). Antenna design using modern additive manufacturing technology: A review. IEEE Access, 8, 177064–177083. Institute of Electrical and Electronics Engineers Inc. https://doi.org/10.1109/ACCESS.2020.3027383

Iida, T., & Wakana, H. (2003). Communications Satellite Systems. Encyclopedia of Physical Science and Technology, 375–408. https://doi.org/10.1016/B0-12-227410-5/00882-6

Im, E., Thomson, M., Fang, H., Pearson, J. C., Moore, J., & Lin, J. K. (2007). Prospects of Large Deployable Reflector Antennas for a New Generation of Geostationary Doppler Weather Radar Satellites.

Kamal, M., & Rizza, G. (2019). Design for metal additive manufacturing for aerospace applications. In Additive Manufacturing for the Aerospace Industry (pp. 67–86). Elsevier Inc. https://doi.org/10.1016/B978-0-12-814062-8.00005-4

Li, M.-J., Li, M., Liu, Y.-F., Geng, X.-Y., & Li, Y.-Y. (2022). A Review on the Development of Spaceborne Membrane Antennas. Space: Science & Technology, 2022, 1–12. https://doi.org/10.34133/2022/9803603

Liu, Z. Q., Qiu, H., Li, X., & Yang, S. L. (2017). Review of Large Spacecraft Deployable Membrane Antenna Structures. Journal of Mechanical Engineering (English Edition), 30(6), 1447–1459. https://doi.org/10.1007/s10033-017-0198-x

Mohanavel, V., Ashraff Ali, K. S., Ranganathan, K., Allen Jeffrey, J., Ravikumar, M. M., & Rajkumar, S. (2021). The roles and applications of additive manufacturing in the aerospace and automobile sector. Materials Today: Proceedings, 47, 405–409. https://doi.org/10.1016/j.matpr.2021.04.596

Najmon, J. C., Raeisi, S., & Tovar, A. (2019). Review of additive manufacturing technologies and applications in the aerospace industry. In Additive Manufacturing for the Aerospace Industry (pp. 7–31). Elsevier Inc. https://doi.org/10.1016/B978-0-12-814062-8.00002-9

Natori, M. C., Katsumata, N., Yamakawa, H., Sakamoto, H., & Kishimoto, N. (2013). CONCEPTUAL MODEL STUDY USING ORIGAMI FOR MEMBRANE SPACE STRUCTURES. http://www.asme.org/about-asme/terms-of-use

Pruett, H. T., Kaddour, A. S., Georgakopoulos, S. V., Howell, L. L., & Magleby, S. P. (2022). Optimizing geometry for EM performance to design volume-efficient Miura-ori for reflectarray antennas. Extreme Mechanics Letters, 56. https://doi.org/10.1016/j.eml.2022.101889

Rismalia, M., Hidajat, S. C., Permana, I. G. R., Hadisujoto, B., Muslimin, M., & Triawan, F. (2019). Infill pattern and density effects on the tensile properties of 3D printed PLA material. Journal of Physics: Conference Series, 1402(4). https://doi.org/10.1088/1742-6596/1402/4/044041

Sankaralingam, S., & Gupta, B. (2010). DEVELOPMENT OF TEXTILE ANTENNAS FOR BODY WEARABLE APPLICATIONS AND INVESTIGATIONS ON THEIR PERFORMANCE UNDER BENT CONDI-TIONS. In Progress In Electromagnetics Research B (Vol. 22).

Shinde, S. D., & Upadhyay, S. H. (2021). The novel design concept for the tensioning system of an inflatable planar membrane reflector. Archive of Applied Mechanics, 91(4), 1233–1246. https://doi.org/10.1007/s00419-020-01841-w

Vertegaal, C., Li, M. J. H., Bentum, M., & Pourshaghaghi, H. R. (2021). Inflatable Coplanar Patch Antenna Array for Spaceborne Applications. IEEE Aerospace Conference Proceedings, 2021-March. https://doi.org/10.1109/AERO50100.2021.9438205

Wang, H. J., Bin, F., Min, Y., Guan, F. L., Liu, G., Xue, C., Xu, Y., Huang, J., Minghui, C., & Shihua, L. (2012). Inflatable antenna for space-borne microwave remote sensing. IEEE Antennas and Propagation Magazine, 54(5), 58–70. https://doi.org/10.1109/MAP.2012.6348118

Xu, Y., & Guan, F. L. (2012). Structure design and mechanical measurement of inflatable antenna. Acta Astronautica, 76, 13–25. https://doi.org/10.1016/j.actaastro.2012.02.005

Yeoh, C. K., Cheah, C. S., Pushpanathan, R., Song, C. C., Tan, M. A., & Teh, P. L. (2020). Effect of infill pattern on mechanical properties of 3D printed PLA and cPLA. IOP Conference Series: Materials Science and Engineering, 957(1). https://doi.org/10.1088/1757-899X/957/1/012064

Published
2023-12-28
How to Cite
Kori, J., Patnaik, S., Chattopadhyaya, S., Chatternjee, S., & Agarwal, K. (2023). Development of Space-Borne Antenna Reflector via 3D Printing. MIST INTERNATIONAL JOURNAL OF SCIENCE AND TECHNOLOGY, 11(2), 43-51. https://doi.org/10.47981/j.mijst.11(02)2023.431(43-51)
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ARTICLES