ARMY MIL-P-70533 NOTICE 1-1998 PROJECTILE 105MM HE RA XM913 XM927 ROCKET PROPELLANT FOR《XM913 XM927式105 mm火箭助推榴弹(HE RA)用火箭推进剂》.pdf
《ARMY MIL-P-70533 NOTICE 1-1998 PROJECTILE 105MM HE RA XM913 XM927 ROCKET PROPELLANT FOR《XM913 XM927式105 mm火箭助推榴弹(HE RA)用火箭推进剂》.pdf》由会员分享,可在线阅读,更多相关《ARMY MIL-P-70533 NOTICE 1-1998 PROJECTILE 105MM HE RA XM913 XM927 ROCKET PROPELLANT FOR《XM913 XM927式105 mm火箭助推榴弹(HE RA)用火箭推进剂》.pdf(5页珍藏版)》请在麦多课文档分享上搜索。
1、1-P-70533 (b) 9999906 2083752 04T I INCH- POUND I MIL-P-70533 (AR) AMENDMENT 6 18 December 1998 SUPERSEDING AMENDMENT 5 O9 April 1993 MILITARY SPECIFICATION PROJECTILE, 105MM, HE, RA, XM913/XM927 ROCKET PROPELLANT FOR MIL-P-60533 was inactivated after 21 August 1998 for new design. I I This amendmen
2、t forms a part of Military Specification MIL-P-70533 (AR), dated 29 October 1990, and is approved for use by the U.S. Army Armaments, Research, Development and Engineering Center and is available for use by all Departments and Agencies of the Department of Defense. PAGE 1 Title: Change “PROJECTILE”
3、to CARTRIDGE”. Change “XM913” to ”M913“ (and wherever it appears). 2.11 Add to SPECIFICATIONS, MILITARY the following: ”MIL-B-117 - Bags, Sleeves and Tubing” Delete: “MIL-C-70532 - Cartridge Packing”. AMSC NIA 1 of 5 FSC 1315 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unl
4、imited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-70533 (AR) AMENDMENT 6 PAGE 2 2.1.1 Add to STANDARDS, MILITARY the following: “MIL-STD-129 - Marking for Shipment and Storage“ PAGE 3 Inhibitor peel strength: Delete first sentence and rep
5、lace With new requirement: “The average peel strength of the inhibitor/propellant bond at 70 5 F shall be 20 pounds per linear inch (pli) minimum. No individual sample tested shall exhibit a peel strength less than 14 pli during acceptance testing.“ * Table I, Delete in its entirety and replace with
6、 new Table I: “Temperature Pressure Burning Rate (degrees F) (PSI) (inches/second) 70 70 145 -50 1000 2000 2000 1000 0.36 + 0.06 0.47 + 0.08 0.52 + 0.08 0.31 + 0.06“ PAGE 5 Table II, Delete in its entirety and replace with new Table II: “Table II. Mechanical Properties of Propellant Temp. Characteri
7、stic Avg of Single 5 readings Sample reading (minimum) (minimum) -50 Ultimate Strain 16.5% 14.5% “ Modulus of Elasticity 11,000 PSI 10,000 PSI “ Ultimate Stress 455 PSI 440 PSI 72 Ultimate Strain 21% 17% “ Modulus of Elasticity 2,000 PSI 1,800 PSI “ Ultimate Stress 180 Psi 170 Psi “ Strain at Max. S
8、tress 20% 16% 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-70533 (AR) AMENDMENT 6 145 Ultimate Strain 14.4% 13% Modulus of Elasticity 1,600 PSI 1,450 PSI Ultimate Stress 139 PSI 135 PSI“ 3.9.1 Delete in its entirety 3.10 Add: (First Articl
9、e only)“ after title. PAGE 8 Propellant after mixing and curing. Change the conformance Criteria for heat of reaction from 5 each“ to 2 each“. Complete Rocket Grain. Delete “4.5.5./4.4.2.4“ in 2 places And substitute 4.5.6/4.4 -2.3“. PAGE 13 4.4.23 Change the inspection method reference of special 1
10、 From 4.5.5. I to 4.5.6“. Change the conformance criteria Of major 106 from 3.13“ to Level III“. Add the following: 109 Weight of grain .- (3 segments) 100% 3.2 Scale Minor 202 Inhibitor flash ( excess ive ) Level. V 3.7.3.1 Visual“ PAGE 14 4.5.1 Strand burning characteristics of propellant. Change
- 1.请仔细阅读文档,确保文档完整性,对于不预览、不比对内容而直接下载带来的问题本站不予受理。
- 2.下载的文档,不会出现我们的网址水印。
- 3、该文档所得收入(下载+内容+预览)归上传者、原创作者;如果您是本文档原作者,请点此认领!既往收益都归您。
下载文档到电脑,查找使用更方便
10000 积分 0人已下载
下载 | 加入VIP,交流精品资源 |
- 配套讲稿:
如PPT文件的首页显示word图标,表示该PPT已包含配套word讲稿。双击word图标可打开word文档。
- 特殊限制:
部分文档作品中含有的国旗、国徽等图片,仅作为作品整体效果示例展示,禁止商用。设计者仅对作品中独创性部分享有著作权。
- 关 键 词:
- ARMYMILP70533NOTICE11998PROJECTILE105MMHERAXM913XM927ROCKETPROPELLANTFORXM913XM927 105 MM 火箭 助推 榴弹 HERA

链接地址:http://www.mydoc123.com/p-446907.html