收藏
下载资源 加入VIP,免费下载

NAVY MIL-D-18503 NOTICE 1-1996 DETONATOR MK 22 MOD 0《MK 22 MOD 0雷管》.pdf

上传人：花仙子 文档编号：978270 上传时间：2019-03-13 格式：PDF 页数：1 大小：28.89KB
下载 相关 举报
NAVY MIL-D-18503 NOTICE 1-1996 DETONATOR MK 22 MOD 0《MK 22 MOD 0雷管》.pdf_第1页
第1页 / 共1页
亲，该文档总共1页，全部预览完了，如果喜欢就下载吧！
资源描述

- -r 7- MIL-D-18503 NOTICE 1 9999906 2022060 39T NOTICE OF INACTIVATION FOR NEW DESIGN MIL-D- 18503(AS) NOTICE 1 11 September 1996 MILITARY SPECIFICATION DETONATOR MK 22 MOD O This notice should be filed in front of MIL-D-l8503(NOrd), dated 25 April 1955. MIL-D-l8503(AS) is inactive for new design and is no longer used, except for replacement purposes. Preparing activity: Navy - AS AMSC NIA FSC 1375 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 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
  • NASA-TM-X-213-1960 Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1 57 2 14 2 54 and 2 87《当马赫数为1 57 2 .pdf NASA-TM-X-213-1960 Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1 57 2 14 2 54 and 2 87《当马赫数为1 57 2 .pdf
  • NASA-TM-X-2163-1971 Some transonic and supersonic dynamic stability characteristics of a variable-sweep-wing tactical fighter model《可变掠翼战术战斗机模型的一些跨音速和超音速动态稳定特性》.pdf NASA-TM-X-2163-1971 Some transonic and supersonic dynamic stability characteristics of a variable-sweep-wing tactical fighter model《可变掠翼战术战斗机模型的一些跨音速和超音速动态稳定特性》.pdf
  • NASA-TM-X-2284-1971 Stability and control characteristics at Mach numbers 1 60 to 2 86 of a variable-sweep fighter configuration with supercritical airfoil sections《当马赫数为1 60至2 86时.pdf NASA-TM-X-2284-1971 Stability and control characteristics at Mach numbers 1 60 to 2 86 of a variable-sweep fighter configuration with supercritical airfoil sections《当马赫数为1 60至2 86时.pdf
  • NASA-TM-X-2313-1971 Large-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effect《在地面效应中的螺旋桨驱动的偏离气流短距起落模型的大型风洞试验》.pdf NASA-TM-X-2313-1971 Large-scale wind-tunnel tests of a propeller-driven deflected slipstream STOL model in ground effect《在地面效应中的螺旋桨驱动的偏离气流短距起落模型的大型风洞试验》.pdf
  • NASA-TM-X-2555-1972 Supersonic aerodynamic damping and oscillatory stability in pitch and yaw for a model of a variable-sweep fighter airplane with twin vertical tails《带有两个垂直尾翼的可变掠.pdf NASA-TM-X-2555-1972 Supersonic aerodynamic damping and oscillatory stability in pitch and yaw for a model of a variable-sweep fighter airplane with twin vertical tails《带有两个垂直尾翼的可变掠.pdf
  • NASA-TM-X-2917-1974 An investigation of several NACA 1 series axisymmetric inlets at Mach numbers from 0 4 to 1 29《当马赫数为0 4至1 29时 若干NACA第1系列的轴对称进气道研究》.pdf NASA-TM-X-2917-1974 An investigation of several NACA 1 series axisymmetric inlets at Mach numbers from 0 4 to 1 29《当马赫数为0 4至1 29时 若干NACA第1系列的轴对称进气道研究》.pdf
  • NASA-TM-X-3078-1974 Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and uncambere.pdf NASA-TM-X-3078-1974 Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and uncambere.pdf
  • NASA-TM-X-3087-1974 Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 degrees《机翼机身组合在攻角为44时的横向航向稳定特性》.pdf NASA-TM-X-3087-1974 Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 degrees《机翼机身组合在攻角为44时的横向航向稳定特性》.pdf
  • NASA-TM-X-311-1960 A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2 37 2 98 and 3 90 at angles of attack to 90 deg《当马赫数为2.pdf NASA-TM-X-311-1960 A wind-tunnel investigation of the aerodynamic characteristics of bodies of revolution at mach numbers of 2 37 2 98 and 3 90 at angles of attack to 90 deg《当马赫数为2.pdf
    • 相关搜索

    当前位置：首页 > 标准规范 > 国际标准 > 其他

    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