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Experimental research on the resistojet thruster heater

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper describes experimental research on a resistojet type rocket thruster which was built as an actuator in the Attitude Control System of a model space robotic platform. A key element of the thruster is the heater responsible for increasing the temperature of the working medium in the thruster chamber and hence the specific impulse. This parameter describes the performance of the thruster, increases providing – for lower propellant consumption – the same propulsion effect (thrust). A high performance thruster means either total launch mass can be reduced or satellite lifetime increased, which are key commercial factors. During the first phase of the project, 7 different heating chamber designs were examined. The heater is made of resistive wire with resistivity of 9Ω/m. Power is delivered by a dedicated supply system based on supercapacitors with output voltage regulated in the range of 20–70 V. The experimental phase was followed by designing the chamber geometry and the heating element able to deliver both: maximum increase of gas temperature and minimum construction dimensions. Experiments with the optimal design show an increase in temperature of the working gas (air) by about 300 °C giving a 40% increase in specific impulse. The final effect of that is a 40% reduction in mass flow rate while retaining thrust at a nominal level of 1 N.
Rocznik
Strony
29--43
Opis fizyczny
Bibliogr. 14 poz., rys., tab.
Twórcy
autor
  • Warsaw University of Technology, Institute of Heat Engineering, Nowowiejska 21/25, 00-665 Warsaw, Poland
autor
  • Warsaw University of Technology, Institute of Heat Engineering, Nowowiejska 21/25, 00-665 Warsaw, Poland
  • Warsaw University of Technology, Institute of Heat Engineering, Nowowiejska 21/25, 00-665 Warsaw, Poland
Bibliografia
  • [1] Fortescue P.W., Stark J., Swinerd G.: Spacecraft Systems Engineering. Wiley, New York 2003.
  • [2] Ley W., Wittmann K. and Hallmann W.: Handbook of Space Technology. American Institute of Aeronautics and Astronautics, Washington, DC 2009.
  • [3] Sutton G.P. and Biblarz O.: Rocket Propulsion Elements. Wiley, New York 2010.
  • [4] Fouquet M., Sweeting M.: UoSAT-12 Minisatellite for high performance earth observation at low cost. Acta Astronaut. 41(1997), 3, 173–182, https://doi.org/10.1016/S0094-5765(97)00181-1
  • [5] Tyc G., Tulip J., Schulten D., Krischke M., Oxfort M.: The RapidEye mission design. Acta Astronaut. 56(2005), 1–2, 213–219, https://doi.org/10.1016/j.actaastro.2004.09.029
  • [6] Da Silva Curiel A., Boland L., Cooksley J., Bekhti M., Stephens P., Sun W., Sweeting M.: First results from the disaster monitoring constellation (DMC). Acta Astronaut. 56(2005), 1-2, 261–271, https://doi.org/10.1016/j.actaastro.2004.09.026
  • [7] Flores-Abad A., Ma O., Pham K., Ulrich S.: A review of space robotics technologies for on-orbit servicing. Prog. Aerosp. Sci. 68(2014), 1–26, https://doi.org/10.1016/j.paerosci.2014.03.002
  • [8] Shiga D.: Next-generation ion engine sets new thrust record. Daily news, 28 September 2007, https://www.newscientist.com/article/dn12709-next-generationion-engine-sets-new-thrust-record/ (accessed 24 Apr. 2017).
  • [9] Sforza P.M.:Theory of Aerospace Propulsion. A volume in Aerospace Engineering, Butterworth-Heinemann, 2012.
  • [10] Jahn R.G.: Physics of electric propulsion. Dover Publications, 2006.
  • [11] Kindracki J., Tur K., Paszkiewicz P., Mężyk Ł., Boruc Ł., Wolański P.: Experimental research on low-cost cold gas propulsion for a space robot platform. Aerosp. Sci. Technol. 62(2017), 148–157, http://dx.doi.org/10.1016/j.ast.2016.12.001
  • [12] Gibbon D., Baker A., Coxhill I., Sweeting S.M.: The Development of a Family of Resistojet Thruster Propulsion Systems for Small Spacecraft. In: Proc. 17th Ann. AIAA/USU Conf. on Small Satellites, SSC03-IV-8, 14 Aug. 2013.
  • [13] What, when, how Portal: Rockets, Ion Propulsion. http://what-when-how.com/ space-science-and-technology/rockets-ion-propulsion/ (accessed: 28.04.2017).
  • [14] Arcis N., Bulit A., Gollor M., Lionnet P., Treuet J.C., Gomez I.A.: Report D2. 1 Database on EP (and EP-related) technologies and TRL. Rep. EPIC-CNES2.1-RP-D2.1-1.2 (2015).
Uwagi
EN
This research was conducted in the framework of the Applied Research Program project, financed by the National Centre for Research and Development, Poland PBS3/A3/22/2015.
PL
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-d6ac4419-6a96-48e7-9fc2-85e026b24561
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