PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Piston pumps for space rocket engines : review and design

Autorzy
Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
A high-performance space propulsion system normally uses pressure fed systems that drive up propellant tank mass and limit space engine performance and design varieties. In this paper, the particular specifications and designing factors that should be met by rocket engine fuel pumps are demonstrated, and a comparative study is formed on the suitableness of all the necessary kinds of pumps to be used with rocket engines and their applications. Furthermore, the paper describes low cost and high-performance pump technology. This new piston pump has been improved for space applications. Depending on the type of body of this pump, its various parts should be evaluated at the desired pressure and temperature as well as the speed of fluid handling, leakage from the body, and the strength of the parts. Our review results are expressed to give complete awareness of different situations in space rockets.
Rocznik
Strony
49--57
Opis fizyczny
Bibliogr. 22 poz., fot., rys., tab.
Twórcy
  • Department of Aerospace Engineering, İzmir Economic University, Turkey Warsaw Affiliation University
Bibliografia
  • [1] S. Wofford, J. Fred Jue, J. Cook, Space Shuttle Main Engine Design Evolution, 57th Joint Army-Navy-NASA-Air Force Propulsion Meeting / 5th Liquid Propulsion Subcommittee Meeting. Colorado Springs, CO. May 3-7, 2010.
  • [2] R. Biggs, Space Shuttle Main Engine: The First Twenty Years and Beyond. American Astronautical Society History Series, Volume 29. Univelt for American Astronautical Society, San Diego, CA, 2008.
  • [3] E. Betts, R. Frederick, R. A., Jr.: A Historical Systems Study of Liquid Rocket Engine Throttling Capabilities, AIAA Paper 2010-6541, 2010.
  • [4] U. Barske, High Pressure Pumps for Rocket Motors. Rocket Propulsion Department, Wescott. August 2016.
  • [5] R. Albat, G. Langel, O. Haidn, Handbuch der Raumfahrttechnik, Hanser Verlag, 2007.
  • [6] Z. Rosenberg, Xcor tests piston pump-fed rocket engine, August 2016.
  • [7] B. Campen, Liquid oxygen piston pump ready for reusable space flight, April 2017.
  • [8] J.C. whitehead , United States Patent , Patent Number: 5,026,259 , Date of Patent: Jun. 25, 1991.
  • [9] J. C. Whitehead, United States Patent , Patent Number: 5,222,873 , Date of Patent: Jun. 29, 1993.
  • [10] J.C. Whitehead, Propulsion Engineering Study for Small-Scale Mars Missions , UCRL-CR-122442, Univ. of Calif. Lawrence Livermore National Lab,September1995.
  • [11] J. C. Whitehead , MARS ASCENT PROPULSION OPTIONS FOR SMALL SAMPLE RETURN VEHICLE , May 12, 1997.
  • [12] M. A. Corbo and Stearns, Ch. F., Practical design against pump pulsations, Proc. 22nd International Pump Users Symposium, 2005.
  • [13] J.C. Whitehead, Hydrogen Peroxide Gas Generator Cycle with a Reciprocating Pump, AIAA Paper 2002-3702, July 2002.
  • [14] M. Gabermann “Near Frictionless Air Cylinders Provide Precision Pneumatic Motion Control System”, “Power Conversion and Intelligent Motion”, Vol. 21, No. 11, pp. 48-51, 1995.
  • [15] M. Ventura , Novel Concepts for an Advanced Non-Toxic Gas Generator , 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Sacramento, CA, July 9-12, 2006.
  • [16] K. Lohner et al, Design and Development of a Sub-Scale Nitrous Oxide Monopropellant Gas Generator, AIAA 2007-5463, 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, OH, 8-11 July 2007.
  • [17] J. C. Whitehead, "Lightweight Quad Pump for Mars Ascent etc.," Final Report to NASA Mars Technology Program for JPL contract no. 126382, 2007.
  • [18] S. Sasaki, Double Acting Pump Piston Patents, United States Patent, Patent Number: 10632256, Date of Patent: April 28, 2020.
  • [19] [12] X. Rui, Y. Zhao, Numerical simulation and experimental research of flow-induced noise for centrifugal pumps, J. Vibroeng., 18, 622–636, 2016.
  • [20] S. Shim, Y. Park, J. Kim, Development of a rotary clap mechanism for positive-displacement rotary pumps: Kinematic analysis and working principle, J Mech Sci Technol 29, 759–767, 2015.
  • [21] D. Kwak, S. Kwo, Performance Assessment of Electrically Driven Pump-Fed LOX/Kerosene Cycle Rocket Engine: Comparison with Gas Generator Cycle. Aerosp. Sci. Technol., 77, 67–82, 2018.
  • [22] P. Simontacchi, et al, PROMETHEUS: Precursor of New Low-Cost Rocket Engine Family, EUCASS 2019, EUCASS, Madrid, Spain, 2019.
Uwagi
PL
Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-4d3c43fd-e6fc-4322-8eeb-efe555f9ff61
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.