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Ivanov R K

Publications in Math-Net.Ru

  1. Analysis of gusts at the vertical maneuver phase (“Pitchover”) of the carrier-aircraft for the launch vehicle ejection

    Keldysh Institute preprints, 2005, 038
  2. Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch

    Matem. Mod., 17:11 (2005),  25–42


© Steklov Math. Inst. of RAS, 2024