COMBUSTION IRREGULARITIES IN SOLID PROPELLANTS.
Final rept., Aug 62-Aug 63,
UTAH UNIV SALT LAKE CITY DEPT OF CHEMICAL ENGINEERING
Pagination or Media Count:
In studies employing the side-vented end-burner, the participation of the solid phase in acoustic oscillations was quantitatively confirmed and described. In cooperation with other laboratories, the usefulness of the burner for propellant evaluation was demonstrated. Initial experiments in a study of non-acoustic instability were performed. Author
- Combustion and Ignition
- Solid Rocket Propellants