THE HIGHLY EFFECTIVE LOW THRUST ROCKET ENGINES DESIGNING METHODS, BASED ON NUMERICAL SIMULATION OF INTRACHAMBER PROCESSES

Authors

  • S. D. Vaulin Author
  • V. L. Salich Author

Abstract

The mathematical models for defining of the output characteristics and
working processes parameters of the low thrust rocket engines on the components
of the fuel “gas + gas”, “gas + liquid” are presented. Proposed a based on numerical
simulation intrachamber processes methods of designing of the low thrust
rocket engines.

Author Biographies

  • S. D. Vaulin

    The doctor of engineering science, professor, head of a chair of engine for flying vehicle, vice rector of scientific work

  • V. L. Salich

    The candidate of engineering science, doctoral candidate on the chair of engine for flying vehicle

Issue

No. 12 (2012)

Section

Calculation and design