Ignition of Liquid Propellant in the 40mm Gun
Abstract
The tests reported here were conducted to determine the effects produced on the ballistics of a liquid monopropellant round by advancing the point of venting of the primer within the propellant column. The tests were conducted with two case configurations in which the L/D ratios of the propellant columns were approximately 3.4 and 5.0. As the point of venting was advanced, muzzle velocity increased in rounds with the L/D ratio of 5.0, but decreased in those with the L/D ratio of 3.4. The amount of unburned propellant remaining in the case after firing increased in both case configurations. In both configurations, the pressure curves were transformed from curves with two distinct pressure peaks, through stages approximating plateau configurations, to curves with one well defined pressure maximum.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 15, 1954
- Accession Number
- AD0035545
Entities
People
- G. L. Poudrier
- K. H. Crutchfield