LABORATORY TEST REPORT

Transcription

1 Report : BAE Systems (Operations) Limited The Faraday Test Centre Marconi Way Rochester Kent ME1 2XX Telephone: Facsimile: TOTAL NUMBER OF PAGES:- 6 LABORATORY TEST REPORT ISSUE: 2 A/L: - DATE: May 2012 CUSTOMER NAME: Panasonic Manufacturing (UK) Ltd, Wharfdale Road, Pentwyn Industrial Estate, Cardiff, CF23 7XB. ITEM TESTED: TYPE NUMBER: SERIAL NUMBER: NATURE OF TEST Personal Computer 4 off CF-D1AVB01F3 1KTCA02544, 1KTCA02160, 1KTCA02431 & 1KTCA02432 Environmental Tests Various (See Tables 1 to 4 of this Report) CUSTOMER ORDER No: & TEST INITIATED: 4 April 2012 TEST COMPLETED: 21 May 2012 COMPILED BY: J. M. Carley 23 May 2012 Senior Qualification Engineer Signature Date APPROVED BY: N. D. Moore 23 May 2012 Senior Qualification Engineer Signature Date THIS DOCUMENT IS SUPPLIED BY BAE SYSTEMS (OPERATIONS) LIMITED ROCHESTER ON THE EXPRESS TERMS THAT IT MAY ONLY BE COPIED IN ITS ENTIRETY AND PARTS SHALL NOT BE COPIED EXCEPT WITH THE PRIOR APPROVAL OF THE LABORATORY THE TEST RESULTS CONTAINED IN THIS REPORT RELATE ONLY TO THE ITEMS TESTED. 1

2 1. SUMMARY 1.1 Personal Computer Part No. CF-D1AVB01F3, Serial No. 1KTCA02544 was subjected to the Environmental Tests detailed in Table 1 below: - Table 1 Low Pressure (Altitude) Storage/Air Transport and Operation/Air Carriage High Temperature - Storage High Temperature - Operation Low Temperature - Storage MIL-STD-810G, Method 500.5, Procedures I and II. Non-Operating, 15,000ft for 1 hour. pre and post this test. Operating, 15,000ft for 1 hour. MIL-STD-810G, Method 501.5, Procedure I. Non Operating, +71 C for thermal pre and post this test. MIL-STD-810G, Method 501.5, Procedure II. Operating, +60 C for thermal MIL-STD-810G, Method 502.5, Procedure I. Non Operating, -51 C for thermal pre and post this test. 4 April April April April

3 Table 1 Contd. Low Temperature - Operation MIL-STD-810G, Method 502.5, Procedure II. Operating, -29 C for thermal Shock Transit Drop MIL-STD-810G, Method 516.6, Procedure IV. The unpowered Unit was subjected to a single drop from a height of 72 onto 2 thick plywood backed by concrete on each of its 6 Faces, 8 edges and the bottom front Left Hand corner with the following observations: - Faces No damage was evident and Unit operated satisfactorily after each drop. Edges After the rear bottom edge, the battery compartment at the front of the Unit opened and the battery was ejected. After re-installing the battery, the Unit operated satisfactorily. After all four Left Hand and Right Hand side edges, the battery compartment at the front of the Unit opened. The compartment was closed and the Unit operated satisfactorily each time. Left Hand Corner After this drop a crack was evident on the inside of the screen. The Unit operated satisfactory. The remaining corner drops were performed on Unit S/No. 1KTCA02160 as per Table 2 of this report. 12 April April

4 1.2 Personal Computer Part No. CF-D1AVB01F3, Serial No. 1KTCA02160 was subjected to the Environmental Tests detailed in Table 2 below: - Table 2 Shock Transit Drop MIL-STD-810G, Method 516.6, Procedure IV The unpowered Unit was subjected to a single drop from a height of 72 onto 2 thick plywood backed by concrete on each of its 8 corners. No damage was evident and Unit operated satisfactorily after each drop. Vibration MIL-STD-810G, Method 514.6, Procedure I. The powered Unit was subjected to random vibration for a duration of 60 minutes in each of its three mutually perpendicular axes at the levels and over the frequency range detailed below: g²/Hz at 12Hz rising to 0.035g²/Hz at 20Hz 0.035g²/Hz between 20 and 40Hz falling to g²/Hz at 200Hz 19 April April 2012 to 23 April

5 Table 2 Contd. Vibration MIL-STD-810F, Method 514.5, Procedure I, Category 24, Figure 514.5C-17. The unpowered Unit was subjected to the random vibration profile defined in Figure 514.5C-17 of MIL-STD-810F for a duration of 60 minutes in each of its three mutually perpendicular axes in turn. on completion of each axis. Functional Shock MIL-STD-810F, Method 516.5, Procedure I, Table II, Ground Equipment. The powered Unit was subjected to 3 shocks of 40g peak acceleration, 11ms pulse duration and terminal peak sawtooth pulse shape in each direction of its three mutually perpendicular axes (18 shocks total). Shock Transit Drop MIL-STD-810F, Method 516.5, Procedure IV The unpowered Unit installed in its shipping package was subjected to a single drop from a height of 72 onto 2 thick plywood backed by concrete on each of its 6 faces, 8 edges and 8 corners. No damage was evident and Unit operated satisfactorily on completion of the test. 23 April April April

6 1.3 Personal Computer Part No. CF-D1AVB01F3, Serial No. 1KTCA02431 was subjected to the Environmental Test detailed in Table 3 below: - Table 3 Humidity MIL-STD-810F, Method on completion of the 5 th cycle, 10 th cycle and on completion of the test. 8 May 2012 to 21 May Personal Computer Part No. CF-D1AVB01F3, Serial No. 1KTCA02432 was subjected to the Environmental Test detailed in Table 4 below: - Table 4 Humidity MIL-STD-810G, Method 507.5, Procedure II - Aggravated on completion of the 5 th cycle, 10 th cycle and on completion of the test. 8 May 2012 to 21 May All of the testing detailed in Tables 1 to 4 of this report was performed at the Faraday Test Centre, BAE Systems (Operations) Ltd, Marconi Way, Rochester, Kent, ME1 2XX (UKAS Accreditation 0047). The Certificates of Laboratory Test relating to these tests are held electronically by Panasonic Manufacturing (UK) Ltd and by BAE Systems. 6