In-Flight Sensor Phase I.
Abstract
The report describes a 6-month effort to investigate a simple, low-cost, all-mechanical in-flight fractional-g sensor designed to provide a second safety feature for mortar fuze safety and arming devices. Work done under a prior contract in this area is reviewed, as well as the design, operation, and performance of two demonstration models fitted to the S+A device from the M532 proximity fuze for the 81mm mortar. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1971
- Accession Number
- AD0734424
Entities
People
- Stanley A. Grapp
Organizations
- Honeywell International, Inc.