The work was carried out at the request of FSUE "GNPP SPLAV", 2002.

The aim of this work was the development of a parametrized model of a nonrigid rocket to conduct research on its dynamic behavior during flight and exit from the launcher. The developed model is used to assess the accuracy of firing and the development of various technical solutions that ensure the stabilization of the projectile during the flight.

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Latest news

Euler version 12.12

A new version of the software package has been released
EULER 12.12 
The demo version 12.12.03 of the software package is available at the link

DOWNLOAD the demo version of EULER

May, 2023

Версия Euler 12.12

Выпущена новая версия программного комплекса
EULER 12.12

Май, 2023

Update of the EULER software package - version 12 has been released

We continue to actively work on improving the EULER software package.

A big update of the software package - the 12th version of EULER has been released, in which the following important changes have been made:

  • a new computational core with significantly expanded capabilities has been developed;
  • increased calculation speed;
  • implicit integration methods are implemented, the use of which reduces the calculation time of rigid systems by orders of magnitude;
  • a number of user interface improvements have been made.
Euler version 11.14

A new version of the EULER 11.14 software package has been released

December, 2020