درباره ما
MS9025 REV A
CLAMP - LOOP TYPE SUPPORT (HEAT RESISTANT) .265 HOLE
Year: 1968
Abstract: This military standard is approved by the Department of Defense and is mandatory on all activities. Selection for all new engineering and design applications and for repetitive use shall be made from this document. ![DIAGRAM]()
MATERIAL: CORROSION RESISTANT STEEL AMS5510.
REMOVE BURRS AND SHARP EDGES.
DIMENSIONS IN INCHES.
CLAMP SHALL BE FORMED AS SHOWN. DIMENSION "D" SHALL FALL WITHIN THE SPECIFIED LIMITS WHEN CLAMP IS ASSEMBLED ON A BAR THE DIA OF WHICH IS EQUAL TO THE NOMINAL TUBE OD WITHIN ±.001.
HOLES SHALL BE IN ALIGNMENT WITHIN .010 AND CLAMP SHALL BE FLAT WITHIN .010 THRU CLAMP WIDTH WHEN ASSEMBLED OR TEST BAR. IN THE FREE POSITION CLAMP RAY SPRING OPEN PROVIDED THE CONDITIONS ARE MET.
DO NOT USE UNASSIGNED PART NUMBERS.
[A circled]AMS IS A SOCIETY OF AUTOMOTIVE ENGINEERS, INC. PUBLICATION.
THIS MILITARY STANDARD WAS DEVELOPED COOPERATIVELY WITH THE MILITARY SERVICES BY THE SAE AEROSPACE PROPULSION DIVISION.
[A circled] NOM A F APPROX PART FIIN TUBE DIA B C D E RAD WEIGHT NO. OD BASIC ±.005 ±.010 REP ±.016 LBS, EA. -------------------------------------------------------------------------------------- MS9025-01 .125 .125 .031 .360 .062-.078 0 .062 .0055 MS9025-02 .188 .188 .031 .423 .062-.078 .031 .062 .0066 MS9025-03 .250 .250 .031 .457 .062-.078 .062 .062 .0075 MS9025-04 .312 .312 .031 .498 .062-.078 .094 .062 .0085 MS9025-05 .375 .375 .031 .529 .062-.078 .125 .062 .0094 MS9025-06 .438 .438 .031 .560 .062-.078 .156 .062 .0103 MS9025-07 .500 .500 .031 .592 .062-.078 .188 .062 .0112 MS9025-08 .562 .562 .031 .623 .062-.078 .219 .062 .0122 MS9025-09 .625 .625 .031 .654 .062-.078 .250 .062 .0131 MS9025-10 .688 .688 .051 .752 .062-.078 .281 .109 .0237 MS9025-11 .750 .750 .051 .783 .062-.078 .312 .109 .0252 MS9025-12 .812 .812 .051 .814 .062-.078 .344 .109 .0267 MS9025-13 .875 .875 .051 .845 .062-.078 .375 .109 .0283 MS9025-14 .938 .938 .051 .877 .062-.078 .406 .109 .0298 MS9025-15 1.000 1.000 .051 .908 .062-.078 .438 .109 .0313 MS9025-16 1.062 1.062 .051 .939 .062-.078 .469 .109 .0331 MS9025-17 1.125 1.125 .051 .970 .062-.078 .500 .109 .0343 MS9025-18 1.188 1.188 .051 1.002 .062-.078 .531 .109 .0359 MS9025-19 1.250 1.250 .064 1.062 .094-.110 .531 .125 .0471 MS9025-20 1.312 1.312 .064 1.093 .094-.110 .562 .125 .0490 MS9025-21 1.375 1.375 .064 1.125 .094-.110 .594 .125 .0509 MS9025-22 1.438 1.438 .064 1.156 .094-.110 .625 .125 .0528 MS9025-23 1.500 1.500 .064 1.188 .094-.110 .656 .125 .0547 MS9025-24 1.562 1.562 .064 1.219 .094-.110 .688 .125 .0566 MS9025-25 1.625 1.625 .064 1.250 .094-.110 .719 .125 .0585 MS9025-26 1.750 1.750 .064 1.312 .094-.125 .781 .125 .0623 MS9025-27 1.875 1.875 .064 1.375 .094 .125 .844 .125 .0661 MS9025-28 2.000 2.000 .064 1.438 .094-.125 .906 .125 .0696
MATERIAL: CORROSION RESISTANT STEEL AMS5510.
REMOVE BURRS AND SHARP EDGES.
DIMENSIONS IN INCHES.
CLAMP SHALL BE FORMED AS SHOWN. DIMENSION "D" SHALL FALL WITHIN THE SPECIFIED LIMITS WHEN CLAMP IS ASSEMBLED ON A BAR THE DIA OF WHICH IS EQUAL TO THE NOMINAL TUBE OD WITHIN ±.001.
HOLES SHALL BE IN ALIGNMENT WITHIN .010 AND CLAMP SHALL BE FLAT WITHIN .010 THRU CLAMP WIDTH WHEN ASSEMBLED OR TEST BAR. IN THE FREE POSITION CLAMP RAY SPRING OPEN PROVIDED THE CONDITIONS ARE MET.
DO NOT USE UNASSIGNED PART NUMBERS.
[A circled]AMS IS A SOCIETY OF AUTOMOTIVE ENGINEERS, INC. PUBLICATION.
THIS MILITARY STANDARD WAS DEVELOPED COOPERATIVELY WITH THE MILITARY SERVICES BY THE SAE AEROSPACE PROPULSION DIVISION.
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