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Optimal Topological Design of a Thermal Isolator for a Monopropellant Space Thruster

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Modeling and Optimization in Space Engineering

Part of the book series: Springer Optimization and Its Applications ((SOIA,volume 144))

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Abstract

This work is focused on the study of the thermal-structural behavior of a thermal isolator device employed in a monopropellant thruster for space applications. Engines of this kind are widely used to perform attitude corrections in artificial satellites. Their operating principle is based on the catalytic decomposition of the fuel (hydrazine), producing gasification with a consequent heat generation. These gases are properly conducted to a nozzle to produce thrust. A couple of redundant solenoid on-off electro-valves, in a serial configuration, are used to control the fuel supply system. To avoid leak risk in this system, soft seals are also used. Duration and performance of this kind of engine rely on two main aspects. The first one is the number of cold ignitions. When the engine starts at low temperature conditions, the catalytic bed is subjected to a thermal transient (high gradient—hundreds of∘ C/s) which generates a breakage of grains, causing low size particles to fill the inter-granular spaces, clogging the downstream gas flow. The second aspect to consider in the reduction of the life span is the loss of reliability in the soft seals used in the fuel supply system due to high temperature degradation. Such degradation can drive the module out of service, generate a catastrophic failure in the reactor, or lead to mission stoppage. A thermal isolator is used to protect the seals from a premature degradation due to thermal effects. Its structural design is optimized by using a novelty structural optimization methodology based on topological sensitivity analysis in this work. This analysis allows achieving the best structural configuration that minimizes the temperature field around the seals and also the isolator weight. Finally, a thermal and structural evaluation of the monopropellant thruster is presented in order to validate the structural strength and integrity. Inertial forces due to high G’s are considered in this analysis.

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References

  1. Allaire, G., Jouve, F., Van Goethem, N.: Damage and fracture evolution in brittle materials by shape optimization methods. Chin. J. Comput. Phys. 230(12), 5010–5044 (2011)

    Article  MathSciNet  Google Scholar 

  2. Amstutz, S.: Sensitivity analysis with respect to a local perturbation of the material property. Asymptot. Anal. 49(1–2), 87–108 (2006)

    MathSciNet  MATH  Google Scholar 

  3. Amstutz, S., Andrä, H.: A new algorithm for topology optimization using a level-set method. J. Comput. Phys. 216(2), 573–588 (2006)

    Article  MathSciNet  Google Scholar 

  4. Amstutz, S., Novotny, A.A.: Topological optimization of structures subject to von Mises stress constraints. Struct. Multidiscip. Optim. 41(3), 407–420 (2010)

    Article  MathSciNet  Google Scholar 

  5. Amstutz, S., Giusti, S.M., Novotny, A.A., de Souza Neto, E.A.: Topological derivative for multi-scale linear elasticity models applied to the synthesis of microstructures. Int. J. Numer. Methods Eng. 84, 733–756 (2010)

    Article  MathSciNet  Google Scholar 

  6. Amstutz, S., Novotny, A.A., de Souza Neto, E.A.: Topological derivative-based topology optimization of structures subject to Drucker-Prager stress constraints. Comput. Methods Appl. Mech. Eng. 233–236, 123–136 (2012)

    Article  MathSciNet  Google Scholar 

  7. Cagliolo, C.M., Salomone, J.E., Jazni, J.E., Lagier, J.E.: Analysis of a thermal behaviour of the fuel supply pipe in a low thrust monopropellant engines. In: 4th Argentinian Congress in Space Technology (CATE), Buenos Aires (2007)

    Google Scholar 

  8. Çengel, Y.A., Ghajar, A.J.: Heat and Mass Transfer. Fundamentals and Applications, 4th edn. McGraw Hill, New York (2011)

    Google Scholar 

  9. Emmons, D.L.: Design criteria manual for long-life monopropellant engines. Technical Report AFRPL-TR-77-6, Rocket Research Company, Redmond (1977)

    Google Scholar 

  10. Gagosian, J.: Hydrazine handbook. Technical Report, Rocket Research Company, Redmond (1993)

    Google Scholar 

  11. Giusti, S.M., Novotny, S.M.: Design of bi-metallic devices based on the topological derivative concept. Mech. Res. Commun. 65, 1–8 (2015)

    Article  Google Scholar 

  12. Giusti, S.M., Novotny, A.A., de Souza Neto, E.A., Feijóo, R.A.: Sensitivity of the macroscopic elasticity tensor to topological microstructural changes. J. Mech. Phys. Solids 57(3), 555–570 (2009)

    Article  MathSciNet  Google Scholar 

  13. Giusti, S.M., Novotny, A.A., de Souza Neto, E.A.: Sensitivity of the macroscopic response of elastic microstructures to the insertion of inclusions. Proc. R. Soc. A Math. Phys. Eng. Sci. 466, 1703–1723 (2010)

    Article  MathSciNet  Google Scholar 

  14. Giusti, S.M., Mello, L.M.A., Silva, E.C.N.: Piezoresistive device optimization using topological derivative concepts. Struct. Multidiscip. Optim. 50, 453–464 (2014)

    Article  MathSciNet  Google Scholar 

  15. Giusti, S.M., Ferrer, A., Oliver, J.: Topological sensitivity analysis in heterogeneous anisotropic elasticity problem. Theoretical and computational aspects. Comput. Methods Appl. Mech. Eng. 311, 134–150 (2016)

    Article  Google Scholar 

  16. Giusti, S.M., Mróz, Z., Sokolowski, J., Novotny, A.A.: Topology design of thermomechanical actuators. Struct. Multidiscip. Optim. 55, 1575–1587 (2017)

    Article  MathSciNet  Google Scholar 

  17. Hintermüller, M., Laurain, A.: Multiphase image segmentation and modulation recovery based on shape and topological sensitivity. J. Math. Imaging Vision 35, 1–22 (2009)

    Article  MathSciNet  Google Scholar 

  18. Hintermüller, M., Laurain, A., Novotny, A.A.: Second-order topological expansion for electrical impedance tomography. Adv. Comput. Math. 36(2), 235–265 (2012)

    Article  MathSciNet  Google Scholar 

  19. Lions, J.L., Magenes, E.: Problèmes aux limites non homogènes et applications, vols. 1–2. Dunod, Paris (1968)

    MATH  Google Scholar 

  20. Lopes, C.G., Santos, R.B., Novotny, A.A.: Topological derivative-based topology optimization of structures subject to multiple load-cases. Latin Am. J. Solids Struct. 12, 834–860 (2015)

    Article  Google Scholar 

  21. Nash, S.G., Griva, I., Sofer, A.: Linear and Nonlinear Optimization. Society for Industrial and Applied Mathematics (SIAM), Philadelphia (2009)

    Google Scholar 

  22. Novotny, A.A., Sokołowski, J.: Topological Derivatives in Shape Optimization. Interaction of Mechanics and Mathematics. Springer, Berlin (2013)

    Google Scholar 

  23. Osher, S., Sethian, J.A.: Front propagating with curvature dependent speed: algorithms based on Hamilton-Jacobi formulations. J. Comput. Phys. 78, 12–49 (1988)

    Article  MathSciNet  Google Scholar 

  24. Rao, S.S.: Engineering Optimization. Theory and Practice, 4th edn. Wiley, New Jersey (2009)

    Google Scholar 

  25. Salençon, J.: Handbook of Continuum Mechanics. General Concepts Thermoelasticity. Springer, Berlin (2001)

    Google Scholar 

  26. Sales, V., Novotny, A.A., Rivera, J.M.: Energy change to insertion of inclusions associated with the Reissner-Mindlin plate bending model. Int. J. Solids Struct. 59, 132–139 (2013)

    Article  Google Scholar 

  27. Salomone, J.E., Giusti, S.M., Sanna, A.D., Micheloud, P.D., Manavella, L.: Study and optimization of structural components of low thrust monopropellants engine. In: 3th Argentinian Congress in Mechanical Engineering (CAIM), Buenos Aires (2012)

    Google Scholar 

  28. Salomone, J.E., Lagier, J.E., Cova, W.J.D., Gonzalez, G.J., Yasielski, R.: Development of a monopropellant thruster of 1.5n to control the orbit and attitude of satellites. In: 4th Argentinian Congress in Space Technology (CATE), Buenos Aires (2007)

    Google Scholar 

  29. Salomone, J.E., Giusti, S.M., Sanna, D.A., Gonzalez, G.J., Cova, W.J.D.: Thermostructural simulation and optimization of a monopropellant engine for space application. In: 6th Argentinian Congress in Space Technology (CATE), La Punta (2011)

    Google Scholar 

  30. Sokołowski, J., Żochowski, A.: On the topological derivative in shape optimization. SIAM J. Control Optim. 37(4), 1251–1272 (1999)

    Article  MathSciNet  Google Scholar 

  31. Sutton, G.P.: Rocket Propulsion Elements. Wiley, New York (1963)

    Google Scholar 

  32. Sutton, D.: Hydrazine thrusters for space applications. J. Br. Interplanet. Soc. 25, 537–551 (1972)

    Google Scholar 

  33. Taylor, R.L., Zienkiewicz, O.C.: The Finite Element Method. Volume 1: The Basis, 5th edn. Butterworth-Heinemann, Oxford (2000)

    Google Scholar 

  34. Van Goethem, N., Novotny, A.A.: Crack nucleation sensitivity analysis. Math. Methods Appl. Sci. 33(16), 197–1994 (2010)

    MathSciNet  MATH  Google Scholar 

Download references

Acknowledgements

This research was partially supported by PID-UTN (Research and Development Program of the National Technological University, Argentina) and CONICET (National Council for Scientific and Technical Research, Argentina). The supports of these agencies are gratefully acknowledged.

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Authors and Affiliations

  1. National Technological University, Regional Faculty of Córdoba (UTN/FRC), Research and Development Group in Applied Mechanics (GIDMA), Córdoba, Argentina

    Sebastián Miguel Giusti, Augusto Alejandro Romero & Javier Eduardo Salomone

  2. National Scientific and Technical Research Council (CONICET), Buenos Aires, Argentina

    Sebastián Miguel Giusti & Augusto Alejandro Romero

Authors
  1. Sebastián Miguel Giusti
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  2. Augusto Alejandro Romero
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  3. Javier Eduardo Salomone
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Correspondence to Sebastián Miguel Giusti .

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Editors and Affiliations

  1. Thales Alenia Space, Turin, Italy

    Giorgio Fasano

  2. Department of Industrial and Systems Engineering, Lehigh University , Bethlehem, PA, USA

    János D. Pintér

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Giusti, S.M., Romero, A.A., Salomone, J.E. (2019). Optimal Topological Design of a Thermal Isolator for a Monopropellant Space Thruster. In: Fasano, G., Pintér, J. (eds) Modeling and Optimization in Space Engineering . Springer Optimization and Its Applications, vol 144. Springer, Cham. https://doi.org/10.1007/978-3-030-10501-3_6

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