NAVY MIL-P-25062 B (1)-1971 PARACHUTE RECOVERY SYSTEMS MISSILE AND DRONE GENERAL REQUIREMENTS FOR DEVELOPMENT OF《导弹和无人驾驶飞机降落伞回收系统总的发展要求》.pdf
《NAVY MIL-P-25062 B (1)-1971 PARACHUTE RECOVERY SYSTEMS MISSILE AND DRONE GENERAL REQUIREMENTS FOR DEVELOPMENT OF《导弹和无人驾驶飞机降落伞回收系统总的发展要求》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-P-25062 B (1)-1971 PARACHUTE RECOVERY SYSTEMS MISSILE AND DRONE GENERAL REQUIREMENTS FOR DEVELOPMENT OF《导弹和无人驾驶飞机降落伞回收系统总的发展要求》.pdf(2页珍藏版)》请在麦多课文档分享上搜索。
1、- I- - _. . _ . - - NIL-P-250bZB (I) lib 7777706 0373262 3 *. - -. _ .- . . _- - . MIL-P-25062B . AMENDMENT 1 27 May 1971 MILITARY SPECIFICATION rl PARACHUTE RECOVERY SYSTEMS, MISSILE AND DRONE, - ._. - _- .- - -. _ -. . - - _-_.I _ - _ GENERAL REQUIREMNTS FOR DEVELOPMENT OF _. This amendment forms
2、a part of Military Specification MIL-P-25062B, dated 25 September 1964, and is mandatory for use by all Departments and Agencies of the qepartment of Defense. i - _- _. . - . Page 1, paragraph 2.1: tion Requirements,. Definitions and Classification of Defects for Parachutes“. Under Military Standard
3、s, add “MIL-STD-849 Inspec- _. .- r. I . - Page 2, paragraph -3.4.1: Delete the last sentence. c- , _ - Page 6, paragraph 3.5: Add at end of paragraph: “(Permissible damage to be - _- . specified in the missile and drone system specification.)“ Page 6: Add: ._ - _- _ _ .* i ? I f: “3.5.1 Reliability
4、. Unless otherwise specified by the procuring activity, the demonstrated reliability of the recovery system under the design conditions shall be:$ minimum of 90 percent with a 90 of sufficient number to demonstrate the reliability required.“ .- percent confidence coefficient Tests specified in 4.3.2
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