问题计划的基础 - BOIP

   

    A.描述：多发射，火箭系统（MLRS）M270A1发射器，LIN：Z57250，Boip：E090AA。M270A1的发射器火箭，装甲车安装，M270A1是一个全天候，高度移动，多次发射，间接的防火火箭和导弹系统，安装在改进的布拉德利底盘（M993）上。M270A1发射器包括改进的防火系统（IFC）和改进的发射机械系统（ILMS）。这两个系统是M270发射器的物料更改。主要组件项目是对讲机设置AN / VIC-3。M270A1长度为22英尺5，高9英尺9，高8英尺高，重量为27.2吨。（1）改进的防火系统（IFCS）：MLRS的IFC提供指挥控制，人机和武器/启动器界面，这是指直接和维护M270A1发射器的控制所必需的。IFCS将取代即将发生的过时电子设备，其中开放式架构系统能够支持未来MLRS系列弹药（MFOM）。IFCS由五个可更换单位（LRU）组成。这些LRU由Fire Control Panel（FCP），位置导航单元（PNU），发射器接口单元（LIU），电源开关单元（PSU）和武器接口单元（WIU）组成。 FEATURES INCLUDE REDUCED OPERATIONS AND SUSTAINMENT (O&S) COSTS, IMPROVED COMMAND AND CONTROL, IMPROVED MAN-MACHINE AND WEAPONS INTERFACES, IMPROVED POSITION NAVIGAION, AND EMBEDDED GLOBAL POSITIONING SYSTEM. BUILT IN TEST/BUILT IN TEST EQUIPMENT MAINTENANCE/DIAGNOSTIC TECHNOLOGY WILL BE INCORPORATED IN IFCS. (2) IMPROVED LAUNCHER MECHANICAL SYSTEM (ILMS): THE CURRENT M270 LAUNCHER HAS A TRAVERSE TIME OF 90 SECONDS FROM THE STOWED POSITION TO WORST CASE AIM POINT. THE CURRENT HYDRAULIC LAUNCHER CONTROLLED SYSTEM WILL BE REPLACED WITH A FASTER, MICROPROCESSOR CONTROLLED SYSTEM, THAT WILL MOVE SIMULTANEOUSLY IN BOTH AZIMUTH AND ELEVATION. THIS WILL REDUCE THE TIME FROM STOW TO WORST CASE AIM POINT BY APPROXIMATELY 85%. IT WILL DECREASE THE RELOAD TIME BY APPROXIMATELY 40%. THE ILMS WILL RESULT IN A REDUCTION OF REPAIR PARTS AND WILL LOWER O&S COSTS. ILMS WILL SUPPORT ALL MLRS MFOM. B. CAPABILITIES: MLRS IS A HIGHLY MOBILE ALL WEATHER WEAPON SYSTEM CAPABLE OF RAPID RESPONSE WITH HIGH VOLUME OF INDIRECT FIRE UTILIZING CONVENTIONAL ROCKETS AND MISSILES AGAINST SOFT/HARD, STATIONARY/MOVING TARGETS. C. EMPLOYMENT: MLRS M270A1 LAUNCHERS ARE LOCATED IN DIVISIONAL MLRS BATTERIES AND FA BRIGADE MLRS BATTALIONS. D. BASIS OF ISSUE: ONE PER MLRS SECTION IAW APPROVED ORGANIZATION DESIGNS. (A ONE FOR ONE REPLACEMENT FOR LAUNCHER, ROCKET: ARMORED VEHICLE MOUNTED, LIN: L44894). TOE ALLOCATION AS FOLLOWS: WHEN UNIT ORGANIZED AS 2 X 9 - 9 WHEN UNIT ORGANIZED AS 3 X 9 - 9 WHEN UNIT ORGANIZED AS 3 X 6 - 6 E. POWER REQUIREMENTS: ELECTRICAL/MECHANICAL SYSTEMS OPERATE ON A 24 VOLT DC POWER SUPPLY. F. TRANSPORTATION REQUIREMENTS: THE M270A1 IS A SELF-PROPELLED TRACK VEHICLE. IT IS AIR TRANSPORTABLE BY C141, C17, AND C5 AIRCRAFT. G. PERSONNEL/MAINTENANCE IMPACTS: (1) OPERATOR: (3) 13M MLRS CREWMEMBER (2) MAINTAINERS: (A) UNIT MAINTENANCE: 31U, 63J, 63T. (B) DIRECT SUPPORT MAINTENANCE: 27M, 35E, 44B, 44E, 63G, 63H. (C) GENERAL SUPPORT: 63G, 63H & 35H. H. SPECIAL NOTES: (1) THIS SYSTEM IS APPROPRIATE FOR INCLUSION IN AR 71-32 (ABOI). (2) ASIOE TO THE Z57250 IS THE TEST SET ELECTRONIC SYTEMS: AN/PSM-95 (Z24989). ONE AN/PSM-95 (Z24989) PER MLRS M27A1 LAUNCHER (Z57250). AND ONE AN/PSM-95 (Z24989) PER MAINTENANCE CONTACT TEAM.