z-logo
open-access-imgOpen Access
NUMERICAL STUDY OF DYNAMICS INTRACHAMBER PROCESSES IN SOLID PROPELLANT SUSTAINER TAKING INTO ACCOUNT FLIGHT OVERLOADS. PART 1. CALCULATION METHOD
Author(s) -
Mikhail P. Egorov,
Dmitry Egorov,
С. А. Егоров
Publication year - 2021
Language(s) - English
DOI - 10.15593/2224-9982/2021.64.10
Subject(s) - combustion , propellant , mechanics , nozzle , combustion chamber , thermal conduction , aerospace engineering , thermodynamics , chemistry , engineering , physics , organic chemistry

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here