ARMY MIL-P-50202 A (7)-1998 PROPELLANT CHARGE ROCKET FOR DEMOLITION KIT CRATERING M180《M180式炸坑爆破包用火箭推进剂药柱》.pdf

上传人:王申宇 文档编号:446456 上传时间:2018-11-16 格式:PDF 页数:2 大小:78.48KB
下载 相关 举报
ARMY MIL-P-50202 A (7)-1998 PROPELLANT CHARGE ROCKET FOR DEMOLITION KIT CRATERING M180《M180式炸坑爆破包用火箭推进剂药柱》.pdf_第1页
第1页 / 共2页
ARMY MIL-P-50202 A (7)-1998 PROPELLANT CHARGE ROCKET FOR DEMOLITION KIT CRATERING M180《M180式炸坑爆破包用火箭推进剂药柱》.pdf_第2页
第2页 / 共2页
亲,该文档总共2页,全部预览完了,如果喜欢就下载吧!
资源描述

1、INCH-POUND MIL-P-502OSA (AR) AMENDMENT 7 27 March 1998 SUPERSEDING AMENDMENT 6 10 June 1988 MILITARY SPECIFICATION PROPELLANT CHARGE, ROCKET, FOR DEMOLITION KIT, CRATERING, M180 This amendment forms a part of MIL-P-50202A(AR), dated 11 April 1977, and is approved for use by the U.S. Army Armament Re

2、search, Development and Engineering Center, and is available for use by all Departments and Agencies of the Department of Defense. PAGE 1 * 2.1, SPECIFICATION, MILITARY: Add new specification as follows: “MIL-STD-105 - Sampling Procedures and Tables For Inspection By Attributes“ PAGE 5 3.1.1: Change

3、 to read: “Propellant. - The propellant shall comply with specification MIL-P-14737, TypeII with the following exceptions: 1. Nitrocellulose content shall be 58.70 2 1.50%. 2. Nitroglycerin content shall be 32.00 2 1.00%. 3. Heat of explosion shall not fall below a minimum of 1250 calories per gram.

4、 PAGE 3 3.5.2: Delete in its entirety. 1 of 2 AMSC N/A FSC 1340 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-P-50202A (7) 9999906 20bbl195 851 = MIL-P-50202A (A

5、R) AMENDMENT 7 3.5.3: Change line 3 to read: less than 900 pound seconds for 0.052 seconds, ma, as determined from thrust curve.“ 3.5.4: Delete in its entirety and substitute with the following: “3.5.4 n im min s 40“E. - The ignition delay time at minus 40F shall not exceed 0.10 second.“ PAGE 9 4.4.

6、2.2: Delete Minor 201 “Protective finish missing or damaged O. 65%, 3.2, Visual“. Change Minor 202 to 201. Major 105: Delete “and angle of head taper“. Add Major 108. Profile of head taper 0.40% - 3.2 - Gage“. PAGE 12 4.4.2.5: Under “Examination or Test“, Major Defect 102, delete: “Action Time . . .

7、 (c) . . . - . . . 3.5.2 . . . 4.5.5.2“. PAGE 14 4.5.5: Line 2, delete: Action Time“. 4.5.5.2: Line 6, delete: “and the Action Time,“. The margins of this amendment are marked with an asterisk or vertical line to indicate where changes (additions, modifications, corrections, deletions) from the prev

8、ious amendment were made. Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous amendment. This was done as a convenience only and the Custodian: Al3IIy-M Preparing activity: Army-AR (Project 1340-1001) 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

展开阅读全文
相关资源
猜你喜欢
  • AECMA PREN 3818-1993 Aerospace Series Bolts with MJ Threads in Titanium Alloy TI-P63 Classification 1 100 MPa (at Ambient Temperature) Technical Specification Edition P 1《航空航天系列TI-.pdf AECMA PREN 3818-1993 Aerospace Series Bolts with MJ Threads in Titanium Alloy TI-P63 Classification 1 100 MPa (at Ambient Temperature) Technical Specification Edition P 1《航空航天系列TI-.pdf
  • AECMA PREN 3819-1992 Aerospace Series Clearance for Wrenches and Sockets Issue P 1《航空航天系列扳手和和插座清理》.pdf AECMA PREN 3819-1992 Aerospace Series Clearance for Wrenches and Sockets Issue P 1《航空航天系列扳手和和插座清理》.pdf
  • AECMA PREN 3820-1999 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Short Thread in Titanium Alloy Anodized MoS2 Lubicated Classification 1 100 MPa (At .pdf AECMA PREN 3820-1999 Aerospace Series Bolts Normal Hexagonal Head Coarse Tolerance Normal Shank Short Thread in Titanium Alloy Anodized MoS2 Lubicated Classification 1 100 MPa (At .pdf
  • AECMA PREN 3821-2009 Aerospace series Washers chamfered with counterbore in heat resisting steel passivated Edition P 2《航空航天系列.钝化耐热钢带埋头直孔的 倒角垫圈.版本P2》.pdf AECMA PREN 3821-2009 Aerospace series Washers chamfered with counterbore in heat resisting steel passivated Edition P 2《航空航天系列.钝化耐热钢带埋头直孔的 倒角垫圈.版本P2》.pdf
  • AECMA PREN 3822-2009 Aerospace series Washers flat thick in heat resisting steel passivated Edition P 2《航空航天系列.钝化耐热钢厚扁平垫圈.版本P2》.pdf AECMA PREN 3822-2009 Aerospace series Washers flat thick in heat resisting steel passivated Edition P 2《航空航天系列.钝化耐热钢厚扁平垫圈.版本P2》.pdf
  • AECMA PREN 3824-1996 Aerospace Series Clinch-Nuts Blind Self-Locking with Counterbore in Corrosion Resisting Steel MoS2 Lubricated Classification 600 MPa (at Ambient Temperature) 3.pdf AECMA PREN 3824-1996 Aerospace Series Clinch-Nuts Blind Self-Locking with Counterbore in Corrosion Resisting Steel MoS2 Lubricated Classification 600 MPa (at Ambient Temperature) 3.pdf
  • AECMA PREN 3825-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 60 IRHD Edition P 1《航空航天系列氟硅酮橡胶硬度60 IRHD P.第1版》.pdf AECMA PREN 3825-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 60 IRHD Edition P 1《航空航天系列氟硅酮橡胶硬度60 IRHD P.第1版》.pdf
  • AECMA PREN 3826-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 70 IRHD Edition P 1《航空航天系列氟硅酮橡胶硬度 70 IRHD P.第1版》.pdf AECMA PREN 3826-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 70 IRHD Edition P 1《航空航天系列氟硅酮橡胶硬度 70 IRHD P.第1版》.pdf
  • AECMA PREN 3827-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 80 IRHD Edition P 1《航空航天系列氟硅酮橡胶硬度 80 IRHD P.第1版》.pdf AECMA PREN 3827-2006 Aerospace series Fluorosilicone rubber (FVMQ) Hardness 80 IRHD Edition P 1《航空航天系列氟硅酮橡胶硬度 80 IRHD P.第1版》.pdf
  • 相关搜索

    当前位置:首页 > 标准规范 > 国际标准 > ARMY

    copyright@ 2008-2019 麦多课文库(www.mydoc123.com)网站版权所有
    备案/许可证编号:苏ICP备17064731号-1