Mil 810E Shock Summary ReportProcedure I – Functional ShockiObjectiveDesigned to represent a shock condition typical of that in operational use. The following conditionsare taken directly from Table 516.4 Mil-STD-810E.iiTest ConditionsMin Peak DurationValue (g’s) (mS)40G11iii QtyMinsamplesConditions2 To be operational.Repeat 3 times foreach axis.Analysis of ResultsPerform Visual and Functional checks before testing sample.Scope plots of Transient shock using appropriate accelerometer.Unit should not glitch or fail during or after each test.No mechanical failure / functional non-conformance of product.ivResultsProduct Code – NV1-4T5GTH-CSerial Number – 8052700003 Unit was taken directly from production. Unit was compliant with production standards.Unit was tested to above procedure, refer to Appendix A for resultsNo mechanical damage or functional failure was observedProduct Code – NV1-4T5GTH-CSerial Number – 8052130010 Unit was taken directly from production. Unit was compliant with production standards.Unit was tested to above procedure, refer to Appendix A for resultsNo mechanical damage or functional failure was observedTEST RESULT - PASSDate Issued: 17/11/05A.IrwinMil 810E Shock Summary ReportLambda UK ConfidentialNV175 Mil 810E Shock ReportPage 1 of 6
Mil 810E Shock Summary ReportProcedure IV – Transit DropvObjectiveDesigned to determine the structural and functional integrity of the unit in its packaged condition.The packaged condition in this case is a single unit packed in an outer cardboard box filled withexpandable foam.viTest ConditionsUsing table 516.4 – II, the product should be dropped according to the following: Drop height 122cmTotal Drops 26.Sample size 5 max.Each corner/edge/ face to be tested 26.1514918132654716171218101911202122232425263Use the following table and the diagram above to complete the drop sequence.Sample No1111111112222222Date Issued: 17/11/05A.IrwinSerial 6700148051670014Surface No13261323241024169718221520Mil 810E Shock Summary ReportLambda UK ConfidentialNV175 Mil 810E Shock ReportPage 2 of 6
Mil 810E Shock Summary Report2333333333vii 14121125171921568Analysis of ResultsConduct visual and functional tests on each sample prior to start.Document impact results (photos if necessary) for each sample.No mechanical failure / functional non-conformance of product.viiiResultsSample 1Product Code – NV1-350FF-N3-CSerial Number – 8051670013 Unit was taken directly from production line. Unit was compliant with production standards.No visible damage to UUT box.No visible damage or audible noise of assemblyUnit PASSED final testSample 2Product Code – NV1-350FF-N3-CSerial Number – 8051670014 Unit was taken directly from production line. Unit was compliant with production standards.No visible damage to UUT box.No visible damage to assembly.Unit PASSED final testSample 3Product Code – NV1-4T5GTHSerial Number – 8052130008 Unit was taken directly from production line. Unit was compliant with production standards.No visible damage to UUT box.No visible damage or audible noise of assemblyUnit PASSED final testTEST RESULT - PASSDate Issued: 17/11/05A.IrwinMil 810E Shock Summary ReportLambda UK ConfidentialNV175 Mil 810E Shock ReportPage 3 of 6
Mil 810E Shock Summary ReportProcedure VI – Bench HandlingixObjectiveDesigned to test the ability of the product to withstand typical bench manual handling duringoperational / servicing use.x Test ConditionsUse a test bench with a thickness of at least 4.25cmWith unit switched off.With the unit sat on its normal side (i.e. with label facing upwards).Lift one end of the unit to 100mm above surface of the bench.Repeat drop 4 times in total.xi Analysis of ResultsConduct visual and functional tests on each sample prior to start.No mechanical failure / functional non-conformance of product.Document the results.xiiResultsProduct Code Serial Number NV1-4T5GTH-C8052130009Unit was taken directly from production line. Unit was compliant with production standards.No visible damage to UUT after tests.No visible damage or audible noise of assembly after tests were observed.Unit PASSED final testTEST RESULT - PASSDate Issued: 17/11/05A.IrwinMil 810E Shock Summary ReportLambda UK ConfidentialNV175 Mil 810E Shock ReportPage 4 of 6
Mil 810E Shock Summary ReportAPPENDIX A – PROCEDURE I RESULTSCLIENT: Lambda UKKingsley AvenueIlfracombeDevonEX34 8ESCERTIFICATE NUMBERSJ200006-001 Issue 1PROJECT NUMBERSJ200006/DHGCLIENT’S ORDER NUMBER967850, dated 3 October 2005INCOMING RELEASE NOTENot released. Delivered on Advice Note 12562DATE OF RECEIPT10 October 2005TEST ITEM(S)Power Supply Units:Type No.Product CodeSerial Nos.NUMBER OF ITEMS TESTEDNV-175NVI-4T5GTH-C2-off NV-175,2-offTEST SPECIFICATION / ISSUEMIL-STD-810EDATE OF TEST28 October 2005TEST(S) APPLIEDShock Test (Functional) to MIL-STD-810E, Method 516.4 Procedure I underthe following conditions:Shock type:Shock test levels:Duration:Number of shocks:Mounting:Function tests:RESULT(S) OF TESTDate Issued: 17/11/05A.Irwin80527000038052130010Terminal peak saw-toothPeak value: 40g11ms3 in each direction of each of the three majororthogonal axes (18 in total)Units attached to a sub base-plate using built-in boltlocationsThe output voltages and currents for each unit to bechecked on completion of shocks in each test axisNo damage to any of the test samples was observed. See ContinuationPage for tabulated results of test measurementsMil 810E Shock Summary ReportLambda UK ConfidentialNV175 Mil 810E Shock ReportPage 5 of 6
Mil 810E Shock Summary ReportTEST HOUSE CERTIFICATE SJ200006-001 Issue 1CONTINUATION PAGERESULT(S) OF TESTNVI-4T56TH-C S/N 8052700003CH1CH2CH3CH4Pre-TestPost 6 ShocksPost 12 3.8323.9523.87A2.52.52.5V11.911.9511.95A222Post 18 Shocks11.89154.771023.832.511.952Pre-TestPost 6 ShocksPost 12 A222Post 18 Shocks11.94154.821024.052.511.812NVI-4T56TH-C S/N 8052130010Date Issued: 17/11/05A.IrwinCH3Mil 810E Shock Summary ReportLambda UK ConfidentialNV175 Mil 810E Shock ReportPage 6 of 6
Mil 810E Shock Summary Report Mil 810E Shock Summary Report NV175 Mil 810E Shock Report Page 1 of 6 Date Issued: 17/11/05 A.Irwin Lambda UK Confidential Procedure I – Functional Shock i Objective Designed to represent a shock condition typical of that in operational use. The following conditions are taken
Texts of Wow Rosh Hashana II 5780 - Congregation Shearith Israel, Atlanta Georgia Wow ׳ג ׳א:׳א תישארב (א) ׃ץרֶָֽאָּהָּ תאֵֵ֥וְּ םִימִַׁ֖שַָּה תאֵֵ֥ םיקִִ֑לֹאֱ ארָָּ֣ Îָּ תישִִׁ֖ארֵ Îְּ(ב) חַורְָּ֣ו ם
Наручные и карманные часы Casio G-Shock GA-100-1A1ER, G-Shock GA-100-1A2ER, G-Shock GA-100-1A4ER, G-Shock GA-100A-7AER, G-Shock . dh Zguo \ . G_ gZ _\Zcl_ wlb Zku \h _fy ieZ\Zgby beb dZdhc - eb[h c vghklb , b c d m Z_lky \ \h m . aZ fb b .
new termination shock and the velocity (V2) of the rarefac-tion wave or weak second shock that propagates down-stream after the interaction of an interplanetary shock with the termination shock. Consider a frame of reference A0 in which the initial termination shock S0 is static. We treat the plasma as an ideal gas whose ratio of specific heats .
Numeric Functional Programming Functional Data Structures Outline 1 Stuff We Covered Last Time Data Types Multi-precision Verification Array Operations Automatic Differentiation Functional Metaprogramming with Templates 2 Numeric Functional Programming Advanced Functional Programming with Templates Functional Data Structures Sparse Data Structures
MANITOU SWINGER REAR SHOCK This Manitou Swinger SPV (Stable Platform Valve) shock is fully assembled and ready to be installed onto your bicycle. Special mounting hardware and a specific shock length is needed for each bicycle. Before riding, take the time to read this manual on set-up, use and service of your shock. SWINGER COIL SPV 6-WAY ADJUST
utilizing high power pulsed lasers to generate shock waves in solid targets, the laser shock technique has led to many investigations, including laser peen-forming (LPF) and laser shock peening (LSP), shown as in Fig. 1. Laser-generated shock waves result from the expansion of a high pressure plasma caused by a pulsed laser.
Plants were then exposed to a heat shock treatment and sampled. As controls, we used well-watered plants (control), drought-stressed plants that were not subjected to heat shock (drought), and well-watered plants that were subjected to heat shock (heat shock). All plants were analyzed and sampled at the same time (after the heat shock treatment).
23. Sharma, P. D. [1991] : The Fungi (Rastogi & Co. Meerut) 24. Vasishta, B. R. [1990] : Fungi (S. Chand & Co. New Delhi) 25. Sharma, O. P. : Fungi (TMH)