Accession Number:

AD0879210

Title:

Feasibility of Non-Destructively Testing Fuze Mechanisms in a Ballistics Range,

Descriptive Note:

Corporate Author:

NAVAL ORDNANCE LAB WHITE OAK MD

Report Date:

1970-10-20

Pagination or Media Count:

21.0

Abstract:

Tests were conducted which demonstrated the feasibility of employing the free-flight technique in a ballistics range to non-destructively test navel ammunition fuze components. Three models containing either an actual or dummy fuze clock were launched in the Naval Ordnance Laboratorys Pressurized Ballistics Range. Each model was launched at 2850 feet per second, a spin rate of 73 revolutions per second, and an axial acceleration loading of 18,000 gs. These conditions simulate those encountered during the firing of a 5338 naval gun. Two models were recovered. One of these contained an actual fuze clock which was recovered virtually undamaged. Average deceleration loading for this recovery was 3000 gs. A wider range of launching conditions can be provided to simulate a great variety of firing simulations. In addition, lower recovery loadings appear practicable. Author

Subject Categories:

  • Ammunition and Explosives

Distribution Statement:

APPROVED FOR PUBLIC RELEASE