NF C90-303-13-1997 Methods of measurement for equipment used in digital microwave radio transmission systems Part 3 measurements on satellite earth stations Section 13 VSAT syste.pdf

上传人:lawfemale396 文档编号:999261 上传时间:2019-03-18 格式:PDF 页数:26 大小:1.06MB
下载 相关 举报
NF C90-303-13-1997 Methods of measurement for equipment used in digital microwave radio transmission systems Part 3  measurements on satellite earth stations Section 13  VSAT syste.pdf_第1页
第1页 / 共26页
NF C90-303-13-1997 Methods of measurement for equipment used in digital microwave radio transmission systems Part 3  measurements on satellite earth stations Section 13  VSAT syste.pdf_第2页
第2页 / 共26页
NF C90-303-13-1997 Methods of measurement for equipment used in digital microwave radio transmission systems Part 3  measurements on satellite earth stations Section 13  VSAT syste.pdf_第3页
第3页 / 共26页
NF C90-303-13-1997 Methods of measurement for equipment used in digital microwave radio transmission systems Part 3  measurements on satellite earth stations Section 13  VSAT syste.pdf_第4页
第4页 / 共26页
NF C90-303-13-1997 Methods of measurement for equipment used in digital microwave radio transmission systems Part 3  measurements on satellite earth stations Section 13  VSAT syste.pdf_第5页
第5页 / 共26页
点击查看更多>>
资源描述

展开阅读全文
相关资源
猜你喜欢
  • NASA NACA-TN-1677-1948 Experimental and calculated characteristics of several high-aspect-ratio tapered wings incorporating NACA 44-series 230-series and low-drag 64-series airfoil.pdf NASA NACA-TN-1677-1948 Experimental and calculated characteristics of several high-aspect-ratio tapered wings incorporating NACA 44-series 230-series and low-drag 64-series airfoil.pdf
  • NASA NACA-TN-1695-1948 Effect of pressure recovery on the performance of a jet-propelled airplane《压力恢复对喷气推进飞机性能的影响》.pdf NASA NACA-TN-1695-1948 Effect of pressure recovery on the performance of a jet-propelled airplane《压力恢复对喷气推进飞机性能的影响》.pdf
  • NASA NACA-TN-1709-1948 Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone《机舱对掠翼空气动力特性的影响和掠角对机翼的影响.pdf NASA NACA-TN-1709-1948 Investigation of the effects of a nacelle on the aerodynamic characteristics of a swept wing and the effects of sweep on a wing alone《机舱对掠翼空气动力特性的影响和掠角对机翼的影响.pdf
  • NASA NACA-TN-1711-1948 Approximate relations for hinge-moment parameters of control surfaces on swept wings at low Mach numbers《在低马赫数时后掠翼上操纵面铰链力矩参数的近似关系》.pdf NASA NACA-TN-1711-1948 Approximate relations for hinge-moment parameters of control surfaces on swept wings at low Mach numbers《在低马赫数时后掠翼上操纵面铰链力矩参数的近似关系》.pdf
  • NASA NACA-TN-1732-1948 Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings《几何二面角对掠翼低速旋转导数的计算影响》.pdf NASA NACA-TN-1732-1948 Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings《几何二面角对掠翼低速旋转导数的计算影响》.pdf
  • NASA NACA-TN-1738-1948 Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan win.pdf NASA NACA-TN-1738-1948 Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan win.pdf
  • NASA NACA-TN-1743-1948 Flight measurements of the stability control and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-data.pdf NASA NACA-TN-1743-1948 Flight measurements of the stability control and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-data.pdf
  • NASA NACA-TN-1759-1948 Effect of compressibility on normal-force pressure and load characteristics of a tapered wing of NACA 66-series airfoil sections with split flaps《压缩性对带有分裂式襟翼.pdf NASA NACA-TN-1759-1948 Effect of compressibility on normal-force pressure and load characteristics of a tapered wing of NACA 66-series airfoil sections with split flaps《压缩性对带有分裂式襟翼.pdf
  • NASA NACA-TN-1766-1948 Wind-tunnel investigation of effects of tail length on the longitudinal and lateral stability characteristics of a single-propeller airplane model《尾长对单螺旋浆飞机模.pdf NASA NACA-TN-1766-1948 Wind-tunnel investigation of effects of tail length on the longitudinal and lateral stability characteristics of a single-propeller airplane model《尾长对单螺旋浆飞机模.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