This document is intended to be used as a guide for range users requiring a flight termination battery. It will provide the user with guidelines for incorporating technical and safety criteria necessary to describe a power source (battery) which will be compatible with the mission critical needs of a flight termination system (FTS). All batteries used to provide the electrical power for an FTS shall have a proven performance reliability of .999 at the 95 percent confidence level. Performance reliability shall be established through statistically based testing. The battery specification, as a minimum, shall include all of the applicable operational, mechanical, electrical, and environmental characteristics of the FTS. As a final product, any battery to be used with an FTS shall be from those units for which lot-acceptance data is in compliance with the specification and the data evaluation requirements of this document. A quality assurance program, such as MIL-Q-9858, must be invoked in the purchase document and placed in operation concurrent with the qualification program so as to allow its assessment prior to beginning production. (kr)
Flight Termination System Battery Guidelines
1989
24 pages
Report
Keine Angabe
Englisch
Batteries & Components , Avionics , Electric batteries , Instrumentation , Flight control systems , Confidence level , Data management , Documents , Electric power , Environments , Flight , Missions , Power supplies , Procurement , Production , Qualifications , Quality assurance , Reliability , Requirements , Safety , Test and evaluation , FTS(Flight Termination System)
Timed Missile Flight Termination System
NTIS | 1976
|Peacekeeper flight termination ordnance system
AIAA | 1995
|British Library Conference Proceedings | 2013
|Timed Missile Flight Termination System
NTIS | 1976
|