Hot Gas Flow Around Burning Aluminum Particles Near Burning Surface of AP Composite Propellant
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Equations for Composite-Propellant Burning
NTRS | 1983
|Effect of Specific Surface Area of Aluminum on Composite Solid Propellant Burning
Online Contents | 2013
|