News

 Statistics

Number of Journals34
Number of Issues1,306
Number of Articles9,427
Article View9,188,648
PDF Download5,620,937
Farhid, M., Moharram, M., Esmaeili, A., pourtaghi, A. (2024). Design, Manufacturing and Testing of a Resistojet Suitable for Atmospheric Conditions. Electronic and Cyber Defense, 12(2), 141-152.
Morteza Farhid; Moharram Moharram; Arezoo Esmaeili; adel pourtaghi. "Design, Manufacturing and Testing of a Resistojet Suitable for Atmospheric Conditions". Electronic and Cyber Defense, 12, 2, 2024, 141-152.
Farhid, M., Moharram, M., Esmaeili, A., pourtaghi, A. (2024). 'Design, Manufacturing and Testing of a Resistojet Suitable for Atmospheric Conditions', Electronic and Cyber Defense, 12(2), pp. 141-152.
Farhid, M., Moharram, M., Esmaeili, A., pourtaghi, A. Design, Manufacturing and Testing of a Resistojet Suitable for Atmospheric Conditions. Electronic and Cyber Defense, 2024; 12(2): 141-152.

Design, Manufacturing and Testing of a Resistojet Suitable for Atmospheric Conditions

مکانیک سیالات و آیرودینامیک
Article 10, Volume 12, Issue 2 - Serial Number 32, March 2024, Pages 141-152    PDF (1.43 M)
Document Type: Original Article
Authors
Morteza Farhid* 1; Moharram Moharram1; Arezoo Esmaeili2; adel pourtaghi3
1Assistant Professor.Iran Space Research Institute, Tabriz, Iran
2PhD student, Iran Space Research Institute, Tabriz, Iran
3Master's degree, Iran Space Research Institute, Tabriz, Iran
Receive Date: 24 October 2023,  Revise Date: 18 January 2024,  Accept Date: 25 January 2024 
Abstract
The purpose of this paper is to design and manufacture a resistojet thruster based on butane propellant with the ability to perform tests in atmospheric conditions. The important sections for designing of this system are heater and nozzle design. The utilized heater is designed for direct heat transfer and the design of the nozzle is based on the thermodynamic relations governing a converging-diverging nozzle which is suitable for the atmospheric outlet pressure. CFD simulation has also been used to investigate the flow of propellant in the nozzle. In the following, the resistojet thruster was built based on the designing and experimental tests were carried out for its validation. By comparing the functional parameters of the thruster, such as thrust force and specific impulse from the experimental results and thermodynamic relationships, the design of the thruster is validated. Considering the heat exchanger power of 30 watts and also the most optimal conditions, the efficiency of the thruster is 21%, the thrust force is 36 millinewtons and the specific impact is computed as 35.9 seconds.
Keywords
Resistojet; Nozzle; Electrical Heater; Thrust Force; Specific Impulse
References
  1. Gibbon D., and Baker A.M., Development of 50 – 100 milliNewton level thrusters for low cost small spacecraft, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 7-10 July 2002, Indianapolis, Indiana, AIAA 2002-4150.
  2. Gibbon D., and Baker A.M., The design, development and in-flight performance of a low power resistojet thruster, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 20-23 July 2003, Huntsville, Alabama, AIAA 2003-4548.
  3. Gibbon D., and Coxhill I.G., The design, development and in-flight operation of a water resistojet micropropulsion system, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 11 - 14 July 2004, Fort Lauderdale, Florida, AIAA 2004-3798.
  4. Coxhill I.G., and Gibbon D., A xenon resistojet propulsion system for microsatellites, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 10 - 13 July 2005, Tucson, Arizona, AIAA 2005-4260.
  5. Smit P., Resistojet thruster design and development programme, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 9 - 12 July 2006, Sacramento, California, AIAA 2006-5210.
  6. Cifali G., Gregucci S., Andreussi T., and Andrenucci M., Resistojet thrusters for auxiliary propulsion of full electric platforms, 35th International Electric Propulsion Conference Georgia Institute of Technology, Atlanta, Georgia, USA October 8 – 12, 2017, IEPC-2017-371.
  7. Romei F., Grubisic A.N., and Gibbon D., Manufacturing of a high-temperature resistojet heat exchanger by selective laser melting, 138 (2017) 356-368.
  8. Robinson M., Grubisic A., Rempelos G., Romei F., Ogunlesi C., and Ahmed S., Endurance testing of the additively manufactured STAR resistojet, Materials and Design 180 (2019) 107907.
  9. Kindracki J, Paszkiewicz P., and Mezyk L., Resistojet thruster with supercapacitor power source – design and experimental research, Aerospace Science and Technology 92 (2019) 847–857.
  10. Koizumi, Asakawa J., Nakagawa Y., Nishii K., Takao Y., Nakano M., and Funase R., Assessment of micropropulsion system unifying water ion thrusters and water resistojet thrusters, Journal of Spacecraft and Rockets 56(5) (2019) 1400-1408.
  11. Nakagawa Y., Iwakawa A., Kameyama Sh., Kikuchi T., Yaginuma K., Asakawa J., and Koizum H., “On-orbit demonstration of the water resistojet propulsion system on commercial 6U-Sat SPHERE-1 EYE”, Small Satellite Conference, Utah State University, Logan, UT, 2023, SSC23-VI-02.
  12. Romei F., Grubišić A., Lasagna D., and Gibbon D., Multiphysics model validation of resistojets with concentric tubular heat exchanger, 7th European Conference for Aeronautics and Space Sciences (EUCASS), 2017.
  13. Morren W.E., and Stone , Development of a liquid-fed water resistojet, ,NASA Lewis Research Center, 1988
  14. Darfilal D., Khatir M., and Rustem A.A., Resistojet propulsion system for small satellit, 9th International Conference on Recent Advances in Space Technologies (RAST),    Istanbul, Turkey, 2019.
  15. Sutton G.P., and Biblarz O., “Rocket propulsion elements”, Ninth Edition, John Wiley & Sons,
  16. Najjar N.A., Dandotiya D., and Farooq N., “Comparative analysis of K-ε and Spalart-Allmaras turbulence models for compressible flow through a convergent-divergent nozzle”, The International Journal of Engineering and Science, Vol. 2, No. 8, pp: 08-17, 2013.
  17. Spalart P.R. and Allmaras S.R., “A One Equation Turbulence Model for Aerodynamic Flows”, Recherche Aerospatiale, Vol. 1, pp: 5-21, 1994.
  18. Pasandidefar M., and Mohammad A., “Investigation and modification of spalart-allmaras turbulence model and its application to flow over a NACA 0012 airfoil”, Journal of Fluid Mechanics and Aerodynamic, 5, No. 2, pp: 71-81, 2017.
  19. Mankavi and  Moghaddas M. H., “Analysis, Simulation, Development and Test of a Liquified gas thruster for a
    specific micro satellite”, M. Sc. Thesis, Malek- Ashtar University of Tehnology, Department of Aerospace Engineering, 2011 (In Persian).
  20. Dehnad M., Farhid M., Akhbari S., and Esmaeili A., “Investigating the effect of geometrical parameters on the performance of a thrust measurement stand and optimizing its design using Genetic Algorithm”, Journal of Aerospace Mechanics, Vol. 19, No. 1, 2023 (In Persian).
Statistics
Article View: 431
PDF Download: 299