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5962R8954203VGA 参数 Datasheet PDF下载

5962R8954203VGA图片预览
型号: 5962R8954203VGA
PDF下载: 下载PDF文件 查看货源
内容描述: [Aerospace Precision JFET-Input Op Amp]
分类和应用: 放大器
文件页数/大小: 12 页 / 116 K
品牌: ADI [ ADI ]
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1.2.4 Case outlines. The case outlines are as designated in MIL-STD-1835 and as follows:  
Outline letter  
Descriptive designator  
Terminals  
Package style  
G
H
P
MACY1-X8  
GDFP1-F10 or CDFP2-F10  
GDIP1-T8 or CDIP2-T8  
8
10  
8
Can  
Flat pack  
Dual-in-line  
1.2.5 Lead finish. The lead finish is as specified in MIL-PRF-38535 for device classes Q and V or MIL-PRF-38535,  
appendix A for device class M.  
1.3 Absolute maximum ratings. 1/  
Positive supply voltage (+V ) ....................................................................... +22 V dc  
S
Negative supply voltage (-V ) ....................................................................... -22 V dc  
S
Storage temperature range ........................................................................... -65°C to +150°C  
Maximum power dissipation (P ) ................................................................. 500 mW 2/  
D
Differential input voltage ............................................................................... ±40 V  
Input voltage ................................................................................................. ±20 V  
Output short circuit duration .......................................................................... Indefinite  
Lead temperature (soldering, 60 seconds) ................................................... +300°C  
Junction temperature (T ) ............................................................................. +150°C  
J
Thermal resistance, junction-to-case (θ ) ................................................... See MIL-STD-1835  
JC  
Thermal resistance, junction-to-ambient (θ ) 2/  
JA  
Case G ..................................................................................................... 150°C/W  
Case P ..................................................................................................... 119°C/W  
Case H ..................................................................................................... 180°C/W  
1.4 Recommended operating conditions.  
Supply voltage (V ) ...................................................................................... ±15 V  
S
Ambient operating temperature (T ) ............................................................. -55°C to +125°C  
A
1.5 Radiation features.  
Maximum total dose available (dose rate = 50 – 300 rads(Si)/s) ......................... 100 krads(Si) 3/  
2. APPLICABLE DOCUMENTS  
2.1 Government specification, standards, and handbooks. The following specification, standards, and handbooks form a part  
of this drawing to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the  
solicitation or contract.  
1/ Stresses above the absolute maximum rating may cause permanent damage to the device. Extended operation at the  
maximum levels may degrade performance and affect reliability.  
2/ Derate linearly 6.7 mW/°C above T = +75°C for P package; derate linearly 7.1 mW/°C above T = +80°C for G package;  
A
A
derate linearly 5.6 mW/°C above T = +70°C for H package.  
A
3/ These parts may be dose rate sensitive in a space environment and may demonstrate enhanced low dose rate effects.  
Radiation end point limits for the noted parameters are guaranteed only for the conditions as specified in MIL-STD-883,  
method 1019, condition A.  
SIZE  
STANDARD  
5962-89542  
A
MICROCIRCUIT DRAWING  
DLA LAND AND MARITIME  
REVISION LEVEL  
E
SHEET  
COLUMBUS, OHIO 43218-3990  
3
DSCC FORM 2234  
APR 97