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MI L - S TD - 202 - 207 CO NT E N T S PARAGRAPH PAG E FOREW ORD … ………………………………………………………. ii 1. SCOPE 1 1.1 Purpose …… ………………… …………………. …… .. …………. 1 2. APPLICABLE D O C U M EN T S 1 2.2.1 Specificatio n s , s t a ndar ds…

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MIL-STD-202-207
FOREWORD
1. This standard is approved for use by all Departments and Agencies of the Department of Defense.
2. This entire standard has been revised. This revision has resulted in many changes to the format, but the most
significant one is the splitting the document into test methods. See MIL-STD-202 for the change summary.
3. Comments, suggestions, or questions on this document should be emailed to std202@dla.mil or addressed to:
Commander, Defense Logistics Agency, DLA Land and Maritime, ATTN: VAT, P.O. Box 3990, Columbus, OH
432183990. Since contact information can change, you may want to verify the currency of this address
information using the ASSIST Online database at https://assist.dla.mil.
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MIL-STD-202-207
CONTENTS
PARAGRAPH PAGE
FOREWORD………………………………………………………. ii
1. SCOPE 1
1.1 Purpose………………………………………….……..…………. 1
2. APPLICABLE DOCUMENTS 1
2.2.1 Specifications, standards, and handbooks………………….... 1
3. DEFINTIONS 1
4. GENERAL REQUIREMENTS 1
4.1. Precautions………………………………………………………. 1
4.2. Apparatus………………………………………………………. 1
4.3 Anvil plate………………………………………………………. 1
4.4 Hammers……………………….………………………………. 2
4.5 Mounting fixtures………………...………………………………. 2
4.6. Procedure………...…………………..…………………………. 2
4.6.1 Mounting method……………………..…………………………. 2
4.6.2 Anvil-plate bolts and positioning springs………………………. 2
4.6.3 Direction of shock……………………………………….………. 2
4.6.4 Height of hammer drops………….…………………….………. 2
4.6.5 Hammer supports……….…………………….…………………. 2
4.6.6 Electrical load and operating conditions….………..…………. 2
4.6.7 External resilient mountings.…………..…….…………………. 2
5. DETAILED REQUIREMENTS 17
5.1 Measurements ……………………………………..………………. 17
5.2. Summary…………………………………………..…..…………. 17
6. NOTES 17
6.1 Supersession data………………………………………………. 17
FIGURE PAGE
1. High-impact shock-testing apparatus …………………….………..….… 3
2. High-impact shock-testing apparatus (backview) with anvil
plate located for back and top blows……………………………….......... 4
3. Anvil plate of shock-testing apparatus………………………..…….....…. 5
4A. Standard mounting fixtures for electrical-indicating switchboard
meters and other panel-mounted parts……………………………….. 6
4B. Standard mounting fixtures for electrical-indicating switchboard
meters and other panel-mounted parts……………………..…………… 9
5. Standard mounting fixtures for electrical controller parts
(contractors, relays, resistors, etc.)………………………………………. 12
6. Standard mounting fixtures for deck, or platform, mounted parts…...… 14
TABLE PAGE
I. Spacers……………………………………………………………………….. 13
II. Mounting panels…………………………………………………………….. 13
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MIL-STD-202-207
METHOD 207
HIGH IMPACT SHOCK
1. SCOPE
1.1 Purpose. This test is performed for the purpose of determining the ability of various parts to withstand shock of
the same severity as that produced by underwater explosions, collision impacts, near-miss gunfire, blasts caused by
air explosions, and field conditions. Exact simulation of some of the severe shock motions experienced in the field is
difficult to reproduce; however, parts that successfully complete the test of this method have been found to possess
the necessary ruggedness for this use. The test apparatus utilized in this method is the same as that designated as
Shock Testing Machine for Lightweight Equipment in
MIL-S-901, Shock Tests, HI (High-Impact), Shipboard
Machinery, Equipment and Systems, Requirements for. The purpose of this apparatus is to determine the ability of
equipment installed aboard naval ships to withstand shock and still continue to perform its operational function. This
test method is limited to testing of parts weighing not more than 300 pounds.
2. APPLICABLE DOCUMENTS
2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a
part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are
those cited in the solicitation or contract.
DEPARTMENT OF DEFENSE SPECIFICATIONS
MIL-S-901 - Shock Tests, H.I. (High Impact), Shipboard Machinery, Equipment, and Systems,
Requirements For
MIL-DTL-1222 - Studs, Bolts, Screws and Nuts for Applications Where a High Degree Of Reliability Is
Required; General Specification For
MIL-I-24768/14 - Insulation, Plastic, Laminated, Thermosetting, Cotton-Fabric-Base, Phenolic-Resin (FBG)
(Copies of these documents are available online at http://quicksearch.dla.mil)
3. DEFINTIONS
This section not applicable to this standard.
4. GENERAL REQUIREMENTS
4.1. Precautions. The apparatus shall be examined periodically for damage. Any hardware that has become
defective by being deformed or cracked shall be replaced. Particular attention shall be given to the anvil plate which
shall not be bowed more than 1 inch at the center. Proper safeguards shall be taken to protect personnel from
objects that may become loosened and act as projectiles as a result of this test. A sound-warning arrangement shall
be made, for use in alerting personnel in the vicinity of the test of the impending drop of the hammer.
4.2. Apparatus. The apparatus used in this test method shall be as shown on figure 1 and the associated detail
drawings. The parts shall be installed on a mounting fixture which is attached to the anvil plate of the shock-testing
apparatus. A 400-pound hammer shall be dropped from a specified height (see 4.6.4) onto a shock pad located on
the anvil plate. The shock motion is then transmitted by the anvil plate to the parts attached on the mounting fixture.
4.3 Anvil plate. The test apparatus of this method is so constructed that the anvil plate (see figure 3) can be
installed, in sequence, in two positions. By utilizing these two installation positions and separately employing both
hammers of the apparatus shock is applied through the three principal mutually perpendicular axes of the part being
subjected to test. One position is to locate the anvil in such a manner that it will receive blows through the back of the
anvil plate by contact from the horizontal hammer, and blows on the top shock pad of the anvil plate by a drop of the
vertical hammer as shown on figure 2. The other position is as shown on figure 1, whereby the end shock pad is
contacted by the horizontal hammer.
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