1、MIL-STD-1658 NOTICE 3 14 M 7777711 0076207 O . y405 2+*- _- . - This document has been approved for public release and sale; its distribution is unlimited. MIL-STD-l658(OS) ,15 May 1974 MILITARY STANDARD SHIPBOARD GUIDED MISSILE LAUNCHING SYSTEM SAFETY REQUIREMENTS, MINIMUM FSC 1440 THIS DOCUMENT CO
2、NTAINS 18 PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-Lb58 NOTICE 3 24 777772L 0076208 2 I MIL-STD-1658 (OS) 15 May 1974 - DEPARTMENT OF DEFENSE WASHINGTON, D.C. 20301 SHIPBOARD GUIDED MISSILE.LAUNCHING SYSTEM SAFETY REQUIREMENTS,
3、MINIMUM MIL-STD-1658 (OS) 1. Agencies of the Department of Defense. This Military Standard is approved for use by all Departments and 2. Recommended corrections, additions, or deletions should be addressed to the Commanding Officer, Naval Ordnance Station, Standardization Division (592), Indian Head
4、, Maryland 20640. ii P Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-Lb5 NOTICE 3 34 m 7777933 0076207 4 mi r MIL-STD-16 5 8 (OS ) . NOTICE - 1 its distribution is unlimited. 6 September 1974 MILITARY STANDARD SHIPBOARD GUIDED MISSILE LAUNC
5、HING SYSTEM SAFETY REQUIEMENTS, MINIMUM To all holders of MIL-STD-l658(OS): 1. Make the following pen and ink changes to MIL-STD-l658(OS) of 15 May 1974: a. Page 4, paragraph 5.5, line 2: Delete lbe 1“. b. Page 5 , paragraph 5.11: Delete entirely and add the note ISee Notice 1 of 6 September 1974 fo
6、r revised paragraph 5.11“ to reference the following revised paragraph 5.11: 5.11 A system shall be provided for the launcher which restricts pointing of the missile to only those “safe zones“ within launched missile would safely clear ship superstructure and installations, The firing circuit shall
7、be interrupted if the missile is pointing outside the “safe zones“. which the 2. Retain this Notice page and insert before the Table of Contents of MIL-STD-l658(OS) of 15 May 1974. 3. Holders of MIL-STD-l658(OS) will verify that pages have been changed as indicated above. is to be retained by stocki
8、ng points until MIL-STD-1658 is revised or can- celled, as Notices This Notice is a separate publication. Each Notice are not cumulative. Custodian NAVY - OS * U.S. GOVERNMENT PRINTING OFFICE: 1974-603110/1848 Preparing Activity NAVY - OS Project Number 1440-NO42 FSC 1440 Provided by IHSNot for Resa
9、leNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3658 NOTICE 3 34 M 7777733 0076233 6 M 1. 2. 3. 4. 4.1 4.2 4.3 4.4 4.5 4.6 5. 6. 7. MIL-STD-l658(OS) 15 May 1974 CONTENTS SCOPE REFERENCED DO(NMENTS DEFINITIONS GENERAL REQU1E”TS SYSTEM SAFETY PROGRAM PERSONNEL AND EQUIPM
10、ENT ELECTROMAGNETIC RADIATION EXPOSURE ENGINEERING CONTINUITY CHECKOUT SAFETY OBSERVER DETAILED REQUIREMENTS SAFETY TESTING DOCUMENTATION - . - . -. /- _._ iii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-STD-1658 NOTICE 3 1q 7779911 0076234
11、B -I MIL-STD-1658 (OS) 15 May 1974 . :. iv I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3658 NOTICE 3 34 = 7779933 007b235 T W - - - MIL-STD-1658 (OS) 15 May 1974 1 SCOPE 1.1 This standard establishes the minimum safety requirements for
12、ship- board guided missile launching systems. be imposed on launching systems handling missiles containing nuclear war- heads or liquid fuels other than hydrocarbon fuels are not included. Special requkrements which may 1.2 feasible, or cost effective for certain types of launching systems. Waiver o
13、r exemption of any requirement for a particular launching system shall require approval of the Weapon System Explosives Safety Review Board. Some of the requiyements of this standard may not be applicable, 1.3 Some of the requirements (5.1 and 5.10 for example) are necessarily general and will requi
14、re more definition when applied to a specific launching system. in the development specification for the launching system. These more definitive requirements will be included 2 REFERENCED DOCUMENTS 2.1 The following documents of the issue in effect on the date of invitation for bids or request for p
15、roposal to the extent specified herein. form a part of this standard Specifications Military . . MIL-E-2036 - Enclosures for Electric and Electronic Equipment, Naval Shipboard MIL-P-23928 - Panels, Electrical, Power Distribution and Manual Transfer, Circuit Breaker Type (Naval Shipboard Use) Standar
16、ds Military MIL-STD-454 - Standard General Requirements for Electronic Equipment MIL-STD-882 - System Safety Program for Systems and Adsociated Subsystems and Equipment : Requirements for MIL-STD-1385 - Preclusion of Ordnance Hazards in Electro- magnetic Fields; General Requirements for 1 Provided b
17、y IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_- - MIL-STD-1658 NOTICE 3 34 m 9997933 0076236 I MIL-STD-1658 (OS) 15 May 1974 MIL-STD-1472 - Human Engineering Design Criteria for Military Systems, Equipment and Facilities MIL-STD-1522 - Standard General Requ
18、irements for Safe Design and Operation of Pressurized Missile and Space Systems Other Publications OD 30393 - Design Principles and Practices for Controlling Hazards 0.f Electromagnetic Radiation to Ordnance (HERO Design Guide) NAVSHIPS 0902-001-5000 - General Specifications for Ships of the United
19、States Navy OR-11 - Development of Packaging, Handling, Storage and Transportation Systems for Weapons American Conference of Governmental - Documentation of the Industrial Hygienists Threshold Limit Values 3 DEFINITIONS 3.1 Launching System. selects, handles, loads, aims, and fires or ejects the mi
20、ssile. That portion of the missile system which stows, 3.2 Launcher. holds the missile in position for firing or ejection. That portion of the launching system which supports and 3.3 missiles are normally stored. and stowage area are one and the same. Stowage Area. That portion of the launching syst
21、em in which the In some launching systems the launcher 3.4 Ejection System. energy external to the missile. until the missile is some distance from the ship. A system for starting the missile in flight with The missile rocket motor is not ignited 3.5 Deadman. A type of switch or control which requir
22、es a sustained force by the operator to maintain the equipment in the “ON“ or operating state. Release of the control will immediately stop equipment operation or movement. 3.6 Wet Sprinkling System. A system which contains lines prefilled with water up to the sprinkling heads as opposed to a “dry“
23、system which does not contain water beyond the main control valve until activated. 3.7 Umbrella Effect. which are physically located between the sprinkling heads and other The shielding effect caused by motors or missiles 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without
24、 license from IHS-,-,-. MIL-STD-Lb58 NOTICE 3 34 M 7777733 0076237 3 M MIL-STD-l658(OS) 15 May 1974 units stowed in the same compartment. receive the full protective effects of the water in the event of fire or accidental initiation of an ordnance component. “he units so shielded do not 3.8 Water In
25、jection System. A system for injecting a high pressure water stream into the exhaust nozzle or exhaust stream of an inadver- tently ignited rocket motor. 3.9 Waiver. A written authorization from the Naval Ordnance Systems Command which specifically permits deviation from a mandatory regulation or in
26、struction for a limited time pending correction of the deficiency. 3.10 Exemption. A written authorization from the Naval Ordnance Systems Command which specifically permits deviation from a mandatory regulation or instruction. 4 GENERAL REQUIRENF,NTS 4.1 System Safety Program. A system safety progr
27、am shall be initiated during the initial phase of the launching system program and shall con- tinue throughout the life of the launching system. shall satisfy the requirements of MIL-STD-882. The safety program 4.2 Personnel and Equipment. Electrical and mechanical interlocks and safety devices shal
28、l be provided to prevent injury to personnel or damage to system equipment during normal operation and maintenance. Controls and circuits shall be arranged so that operation of any control or combination of controls in other than normal sequence shall not cause injury to personnel, operation of the
29、equipment, or damage to any compo- nent. Power failure shall not initiate equipment or missile motion (e.g., through inadvertent release of latches), create any dangerous condition, or cause damage to the equipment or missiles, Interlocks shall be designed to place the equipment in the safest of the
30、 various possible alternate conditions in case of interlock or power failure. 4.3 Electromagnetic Radiation Exposure. Exposure of the launching system to the electromagnetic radiation environment defined in MIL-STD- 1385 shall not cause initiation of any electro-explosive device in the launching sys
31、tem or result in malfunctioning of the launching system. Guidance for meeting this requirement is contained in OD 30393. 4.4 Human Engineering. The human engineering design safety criteria of MIL-STD-1472 shall be satisfied, 4.5 Continuity Checkout. There shall be no electrical continuity tests of e
32、lectrical initiating elements of the missile warhead, rocket motor or self-destruct device while the missile is in the launching system, 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-STD-365 NOTICE 3 34 7777733 007623 5 M _ I HIL-STD-1658 (O
33、S) 15 May 1974 I I I 4.6 Safety Observer. A safe,ty observers station which provides an unobstructed view of the launcher area by direct or remote vision shall be provided. The safety observer shall have communications with the launching system control station and missile firing officer. observers s
34、tation shall not expose the safety observer to the exhaust of a launched missile. The safety 5 DETAILED REQUIREMENTS 5.1 Within the constraints of weight, space, and cost, the maximum feasible ballistic protection against gunfire, fragments, and shock resulting from enemy action shall be provided. 5
35、.2 for the missile, it shall meet the requirements of OR-11, Appendix A. If a part of the launching system is used as a shipping container 5.3 Means shall be provided to prevent the chain ignition of rocket motors and warheads in case of inadvertent ignition of a rocket motor. Means considered shall
36、 include separation, restraint, venting, flame shields, fragment shields, wet sprinkling systems; water injection systems, and flame tight compartments. 5.4 movement in case of inadvertent ignition of the rocket.motor or shipboard shock conditions. The missile in the launching system shall be restra
37、ined to prevent 5.5 watertight. area doors and hatches are closed during missile launching. Stowage area doors, hatches, and covers shall be flameproof and Interlocks shall be 1 be provided which assure that stowage 5.6 rocket motor ignition. Other missiles in the launching system and in- ternal shi
38、p areas shall not be exposed to the missile exhaust. 5.7 which will effectively relieve abnormal stowage area pressures (resulting from inadvertent ignition of a rocket motor) to a level that can be withstood by the stowage area bulkheads. 5.8 automatic and manual control. The design of this system
39、shall minimize the “umbrella effect“. indication of sprinkling system activation. The missile exhaust shall be vented to the atmosphere in case of A pressure relief system shall be provided for the stowage area The stowage area shall have a “wet“ Sprinkling system with both A detection and alarm sys
40、tem shall provide 5.9 trol system. overheating conditions. The stowage area shall have an internal automatic temperature con- A detection and alarm system shall provide indication of , 4 .- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3658
41、 NOTICE 3 34 = 777773L 0076237 7 I MIL-STD-1658 (OS) 15 May 1974 5.10 The missile shall be protected against the expected environments of shock, vibration, gun blast, green water, salt spray and missile blast. The launching system shall be designed to withstand these environments without sustaining
42、damage. 5.11 to those zones whithin which the launched missile will safely clear all ship structure and installations by interrupting the firing circuit if the missile is pointing outside these zones. A system shall be provided which restricts the launching of the missile 5.12 Means shall be provide
43、d to remotely arm and disarm the rocket motor. 5.13 against access that would allow unauthorized firing of a missile. 5.14 Firing Circuit. The launching system shall have the capability of being secured 5.14.1 of at least three independent failures when there is no power to the firing circuit, and a
44、t least two independent failures when there is power to the firing circuit. An inadvertent firing shall not be possible without the occurrence 5.14.2 is imminent. shall be interrupted. Interlocks shall be provided in the firing circuit to insure proper missile/launching system prelaunch conditions a
45、re satisfied before firing is allowed. The firing circuit to the missile shall be interrupted until firing Both the “hot“ side and return side of the firing circuit 5.14.3 firing circuit nearest to the missile shall be electrically interrupted by an electro-mechanical device such as an open relay co
46、ntact. 5.14.4 The firing circuit shall be electrically balanced: that is; the return shall not be via the chassis. sides shall be isolated from ground. Prior to completion of the firing circuit, the portion of the The firing circuit “hot“ and return 5.14.5 cables in the system in accordance wizh OD
47、30393. by shielding or by the physical separation of the wiring. 5.14.6 board noise and spikes on the power lines due to start up or shut down of heavy equipment, etc. do not inadvertently trigger the firing circuit. All firing circuit wiring sha:L1 be isolated from other wiring and This may be acco
48、mplished Filtering or other techniques shall be used to ensure that ship- 5.15 thrust build-up to clear the ship before the missile is released. The launcher shall have-a mechanism which requires adequate missile 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license
49、from IHS-,-,- - _ . . - .- -. . . - - . _- r MIL-STD-Zb5 NOTICE 3 14 m 77977LL 007b220 3 m MIL-STD-l658(OS) 15 May 1974 5.16 motion of the ship, launcher or missile will not result in unscheduled contact of the aft end of the missile and forward end of the launcher during launch. Sufficient launching clearance shall be pr
