Advertisement

Russian Aeronautics

, Volume 61, Issue 2, pp 299–303 | Cite as

Static Stability in the Angular Motion of an Aircraft with a Laser-Induced Spike Conical Nozzle

  • A. G. Sattarov
  • A. V. SochnevEmail author
  • A. R. Bikmuchev
Technical Notes Flight Vehicle Design
  • 5 Downloads

Abstract

The location of the center of mass closer to the source of radiation during rectilinear accelerated motion of an aircraft in the absence of gravity and drag forces provides stability of the angular motion. The proposed scheme was analyzed on the basis of the Lagrange–Dirichlet theorem.

Keywords

laser rocket jet engine rocket engine laser jet propulsion static stability 

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 1.
    Sergienko, A.A., and Zhou, W., Earth-to-Orbit Space Transportation System, Izv. Vuz. Av. Tekhnika, 2005, vol. 48, no. 2, pp. 21–24 [Russian Aeronautics (Engl. Transl.), vol. 48, no. 2, pp. 30–35].Google Scholar
  2. 2.
    Altunin, K.V., Gortyshov, Yu.F., and Dresvyannikov, F.N., Progress of in the Field of Domestic Rocket-Space Engineering and Cosmism of K.E. Tsiolkovsky, Vestnik KGTU im. A.N. Tupoleva, 2010, no. 4, pp. 208–214.Google Scholar
  3. 3.
    Tsiolkovsky, K.E., Izbrannye trudy (Selected Works), Marov. M.Ya., Ed., Moscow: Nauka, 2007.Google Scholar
  4. 4.
    Sattarov, A.G., A Concept of a Spacecraft with Small Initial Mass Placed in the Near-Earth Orbit by a Laser Rocket Engine, Izv.Vuz. Av. Tekhnika, 2008, vol. 51, no. 2, pp. 41–45 [Russian Aeronautics (Engl.Transl.), vol. 51, no. 2, pp. 166–172].Google Scholar
  5. 5.
    Rezunkov, Yu.A., Laser Reactive Thrust. Review of Research, Opticheskii Zhurnal, 2007, no. 8, pp. 20–32 [Journal of Optical Technology (Engl.Transl.), vol. 74, no. 8, pp. 526–535].Google Scholar
  6. 6.
    Sattarov, A.G., Laser Jet Propulsion Based on the Continuous Optical Discharge, Izv.Vuz. Av. Tekhnika, 2008, vol. 51, no. 3, pp. 46–49 [Russian Aeronautics (Engl.Transl.), vol. 51, no. 3, pp. 293–299].Google Scholar
  7. 7.
    Sattarov, A.G., A Method for Calculating a Temperature Field of Multiple Plasma Formations in the Laser Rocket Engine Absorption Chamber, Izv.Vuz. Av. Tekhnika, 2008, vol. 51, no. 4, pp. 69–71 [Russian Aeronautics (Engl.Transl.), vol. 51, no. 4, pp. 452–456].Google Scholar
  8. 8.
    Sattarov, A.G. and Sochnev, A.V., Research of Laser Exhaust Thrust Components by Means of the Second Order Type Regression Equation, Vestnik KGTU im. A.N. Tupoleva, 2016, no. 1, pp. 32–39.Google Scholar
  9. 9.
    Sattarov, A.G. and Sochnev, A.V., Measurement Duration Pulse of the Optical Discharge in Air and on CHOModel for Evaluation of Power Parameters and Operating Modes of the Pulsed Laser, Trudy Academenergo. 2016, no. 3, pp. 133–140.Google Scholar
  10. 10.
    Sattarov, A.G., Sochnev, A.V. and Bikmuchev, A.R., Measurement of the Momentum Reactive Force Produced by a Pulsed Optical Discharge by Means of a Ballistic Pendulum, Trudy Academenergo, 2015, no. 1, pp. 75–82.Google Scholar
  11. 11.
    Afanas'ev, V.A., Degtyarev, G.L., Meshchanov, A.S., and Sirazetdinov, T.K., Control of Spacecraft Turns in Scheduled Time Using Rocket Engines, Izv.Vuz. Av. Tekhnika, 2013, vol. 56, no. 1, pp. 73–77 [Russian Aeronautics (Engl.Transl.), vol. 56, no. 1, pp. 99–106].Google Scholar
  12. 12.
    Afanas’ev, V.A., Degtyarev, G.L., Meshchanov, A.S., and Sirazetdinov, T.K., Study of Space Rocket Dynamics, Control and Stabilization at Starting from an Accelerator-Aircraft, Izv.Vuz. Av. Tekhnika, 2006, vol. 49, no. 3, pp. 17–22 [Russian Aeronautics (Engl. Transl.), vol. 49, no. 3, pp. 23–31].Google Scholar
  13. 13.
    Syzdykov, E.K. and Gainutdinova, A.V., Design Calculation of Light Piston-Engined Aircraft Controllability and Stability Parameters, Izv.Vuz. Av. Tekhnika, 2010, vol. 53, no. 2, pp. 12–15 [Russian Aeronautics (Engl.Transl.), vol. 53, no. 2, pp. 134–140].Google Scholar
  14. 14.
    Michaelis, M.M. and Forbes, A., Laser Propulsion: a Review, South African Journal of Science, 2006, vol. 102, nos. 7–8, pp. 289–295.Google Scholar
  15. 15.
    Myrabo, L.N., World Record Flights of Beam-Riding Rocket Lightcraft: Demonstration of “Disruptive” Propulsion Technology, Proc. of the 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2001, AIAA 2001–3798.Google Scholar
  16. 16.
    Ageichik, A.A., Egorov, M.S., Rezunkov, Yu.A., Safronov, A.L., and Stepanov, V.V., RU Patent no. 2266420, Byul. Izobret., 2005, no.35.Google Scholar
  17. 17.
    Phipps, C., Birkan, M., Bohn, W., Eckel, H.A., Hideyuki Horisawa, Lippert, T., Rezunkov, Yu., et al., Review: Laser-Ablation Propulsion, Journal of Propulsion and Power, 2010, vol. 26, no. 4, pp. 609–637.CrossRefGoogle Scholar

Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • A. G. Sattarov
    • 1
  • A. V. Sochnev
    • 1
    Email author
  • A. R. Bikmuchev
    • 2
  1. 1.Tupolev Kazan National Research Technical UniversityKazanRussia
  2. 2.Gagarin Research and Test Cosmonaut Training CenterZvesdnyi gorodok, Moskovskaya oblastRussia

Personalised recommendations