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


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.


laser rocket jet engine rocket engine laser jet propulsion static stability 


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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

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