Electro-mechanic fuze for rockets
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Abstract
The design of fuze in this research use the methodology and procedures indicated in MIL-STD-1316D which determined the safety qualifications need to be considered when designing fuze. This design incorporates both mechanical and electrical mechanisms for target perception, conditions and command responses that are pre-determined for safe and accurate detonation of the fuze. Also, patents are studied as guidelines for designing and developing of the fuze to further enhanced safety and potential of the fuze. This research article is a report of the design and simulation of Electri-mechanic fuze to use as a foundation for further studies in the future.
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References
Department of Defense, (1991). Military Standard Fuze Design, Safety Criteria For. Avialable at http://www.everyspec.com
Military and Government Specs & Standards. 2012. Standard practical system safety. MIL-STD-882 Revision E, Naval Publications and Form Center (NPFC). 104p.
Department of Defense, 1991. MIL-STD-1316D, Military standard: fuze design, safety criteria for. 21p.
Filo, G. F., Kurschner, D. L. and Weber, P. L. (1993). Elecro-mechanical base element fuze. United States Patent. US5271327. Date of Patent: 21 December 1993. 13p.
Sutcliffe, S. A. (2007). Modular electronic fuze. United States Patent. US 7,213,518 B2. Date of Patent: 8 May 2007. 3p.
James J.O., (1973). Arming Device for Missiles. United States Patent. US 3,722,419.
ณรงค์ ทองฉิม และเจริญ วงษ์ชุ่มเย็น. (2552). ออกแบบไอซีดิจิทัลด้วย FPGA และ CPLD ภาคปฏิบัติโดย ใช้ภาษา VHDL. พิมพ์ครั้งที่ 1. ซีเอ็ดยูเคชั่น, บมจ. 440น.
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