Memorandum report. Army Ballistic Research Lab Aberdeen Proving Ground, MD, 1961, - 299 p.Thermodynamic properties of all commonly used military gun propellants plus some experimental propellants are presented in tabular and graphical form. For the military propellants, these properties are given over a loading density ranging from 0.05 to 0.4 gm/cc. Comparisons are made between the propellants on the basis of force and isochoric flame temperature. The tables and data presented herein can be used for gun design computations.Contents:
Introduction.
Соmputational results.
Miscellaneous computations.
Thermodynamic data.
Discussion.
