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Investigation of an additional oxidizer charge effect on selected operational characteristics of a solid-fuel rocket engine

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper has been intended to discuss some issues closely related to the elimination of an extremely disadvantageous phenomenon, i.e. the occurrence of a negative oxygen balance in products of combustion emitted by a solid-fuel rocket engine while launching a missile from the aircraft. Findings of experimental examination of such engines furnished with an additional oxidizer charge have also been presented.
Rocznik
Strony
139--149
Opis fizyczny
Bibliogr. 18 poz., rys., tab.
Twórcy
autor
  • Air Force Institute of Technology, Warsaw, Poland
  • Air Force Institute of Technology, Warsaw, Poland
Bibliografia
  • 1. Bagrowski J., Kamiński R., 2011, Development of the process to Manufacture the K2SO4 Salt Charges for Rocket Engines in Polish), Instytut Techniczny Wojsk Lotniczych (ITWL), Warszawa
  • 2. Bagrowski J., Kamiński R., Klemba T., 2011, On the Impact of the Nitrocellulose Nitrification Degree on the Oxygen Balance of the Rocket Propellant; Determination of Physical and Chemical Parameters of Combustion Products (in Polish), Instytut Techniczny Wojsk Lotniczych (ITWL), Warszawa
  • 3. Gajewski S.A., Morozov F.N., Tikhomirov J.P., 1980, Automatics for Aircraft Gas Turbine Power Systems (in Russian), Voennoe Izdatelstvo Ministerstva Oborony SSSR, Moskva
  • 4. Hawley E., 2003, Mk66 Rocket Motor/Helicopter Compatibility Program, Indian Head Division
  • 5. Kowalski M., Pietraszek M., Szymczak J., Winczura Z., 2011, Analysis of the Aircraft Engine Stall/Surge in the Course of Launching the NLPR-700 Rockets from the W-3W Helicopter, (in Polish), Instytut Techniczny Wojsk Lotniczych (ITWL), Warszawa
  • 6. KurowW., Dołżański J., 1964, Principles Behind the Solid-Propellant Rocket Design (in Polish), Wydawnictwo MON, Warszawa
  • 7. Leciejewski Z., 2010, Analysis and Assessment of Correctness of Methods of Pyrostatic Testing of Single- and Double-Based Powders (in Polish), Wojskowa Akademia Techniczna (WAT), Warszawa
  • 8. Lubieniecka J., Łukasiewicz J., 2011, Report No. S-1/16/2011 on examination/testing of 02.000”R1” power plants of uncontrolled air-launched rockets (NLPR-70) (in Polish), Instytut Techniczny Wojsk Lotniczych (ITWL), Warszawa
  • 9. Lubieniecka J., Łukasiewicz J., Tchórznicki K., 2013, Report No. S-1/16/2011 on examination/testing of power plants furnished with K2SO4 charges in uncontrolled air-launched rockets (NLPR-70), (in Polish), Instytut Techniczny Wojsk Lotniczych (ITWL), Warszawa
  • 10. Niechaev J.N., Fiedorov R., et al., 1980, Theory of Aircraft Engines (in Russian), Voennoe Izdatelstvo Ministerstva Oborony SSSR, Moskva
  • 11. NO-10-A232:2009 Uzbrojenie lotnicze. Balistyka wewnętrzna silnikow rakietowych. Badania naziemne (Air weapons. Interior ballistics of rocket engines. Ground tests)
  • 12. Operation Manuals for Helicopters (in Polish): – Mi-24A and Mi-24D helicopters, practical aerodynamics, Lo 2011/80, Poznań 1980 – Turbojet aircraft engine TW3-117MT series 3, Technical description and maintenance guidelines, Lot 2855/90, Poznań 1991 – Turbojet engine TWD-10B, Maintenance Manual, Doc. No. 19.0.646 (10B.00.030.RE2), WSK-Rzeszow, 1984
  • 13. Romasiewicz W.F., Samoilow G., 1980, Practical Helicopter Aerodynamics (in Russian), Voennoe Izdatelstvo Ministerstva Oborony SSSR, Moskva
  • 14. Safta D., Vasile T., Ion I., 2011, Regarding the influence of high frequency combustion instabilities on operation of solid rocket motors, Problems of Mechatronics. Armament Aviation, Safety Engineering, 1, 3, 7-24
  • 15. Stieczkin B.S., Kazandżan P.K., Aleksiejew Ł.P., Goworow A.N., Konowałow N.E., Nieczajew J.N., Fiodorow R.N., 1961, Theory of Aircraft Engines (in Polish), Wydawnictwo MON, Warszawa
  • 16. Torecki S., 1989, Interior Ballistics of Solid-Propellant Rocket Engines (in Polish), Wojskowa Akademia Techniczna (WAT), Warszawa
  • 17. Yang V., Brill T., Ren W., 2000, Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, American Institute of Aeronautics and Astronautics, Virginia
  • 18. Żyluk A., 2009, Simulation Tests of Exterior Ballistics Demonstrated by Air Weapons (in Polish), Instytut Techniczny Wojsk Lotniczych (ITWL), Warszawa
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-df882dc2-1262-4e77-9761-182d80e80a6c
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