RTAX-S FIELD PROGRAMMABLE GATE ARRAY (FPGA) RISK REDUCTION TESTING - NESC ACTIVITY 06-010-E INTRODUCTION/BA…

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RTAX-S FIELD PROGRAMMABLE GATE ARRAY (FPGA) RISK REDUCTION TESTING - NESC ACTIVITY 06-010-E INTRODUCTION/BACKGROUND: THE TESTING DESCRIBED BY THE STATEMENT OF WORK (SOW) IS IN SUPPORT OF A RISK ASSESSMENT COMMISSIONED BY THE NASA ENGINEERING AND SAFETY CENTER (NESC). THE EVALUATION LIFE TESTING SHALL BE PERFORMED ON 160 FPGA S: 80 PARTS OF ACTEL RTAX250S -CQ208 AND 80 PARTS OF ACTEL RTAX2000S -LG624. THE TESTING SHALL INCLUDE 6000 HOURS TOTAL OPERATING TIME WITH A HALT IN OPERATION AND PART EVALUATION EVERY 500 HOURS. THE TESTING SHALL BE PERFORMED ACCORDING TO THE FOLLOWING PARAMETERS: TABLE 1 - LIFE TEST PROFILE HOURS TEMPERATURE CORE VOLTAGE 500 HTOL NOMINAL (1.5V) 500 LTOL 1.425V (LOW) PULL FOR ATE TEST 500 HTOL 1.575V (HIGH) 500 LTOL NOMINAL (1.5V) PULL FOR ATE TEST 500 HTOL 1.425V (LOW) 500 LTOL 1.575V (HIGH) PULL FOR ATE TEST 500 HTOL NOMINAL (1.5V) 500 LTOL 1.425V (LOW) PULL FOR ATE TEST 500 HTOL 1.575V (HIGH) 500 LTOL NOMINAL (1.5V) PULL FOR ATE TEST 500 HTOL 1.425V (LOW) 500 LTOL 1.575V (HIGH) PULL FOR ATE TEST HTOL IS DEFINED AS HIGH TEMPERATURE OPERATING LIFE, AND SHALL BE SET TO ACHIEVE A JUNCTION TEMPERATURE OF 125 DEG C. LTOL IS DEFINED AS LOW TEMPERATURE OPERATING LIFE, AND SHALL BE SET TO -55 DEG C CHAMBER TEMPERATURE. ATE IS DEFINED AS AUTOMATED TEST EQUIPMENT - PULL FOR ATE TEST IS DESCRIBED IN TASK 4 BELOW. DESCRIPTION OF TASKS TO BE PERFORMED: THE CONTRACTOR SHALL PROVIDE THE NECESSARY FACILITIES, FIXTURES, MANPOWER AND EXPERTISE TO PERFORM THE FOLLOWING: 1. PERFORM 6000 HOURS OF ENVIRONMENTAL TESTING IN ACCORDANCE WITH THE PARAMATERS SET FORTH IN LIFE TEST PROFILE OUTLINED IN TABLE 1. 2. PROVIDE EXISTING ACTEL BURN-IN BOARDS COMPATIBLE WITH THE 160 PARTS PROVIDED BY NASA FOR THIS TESTING, FOR THE DURATION OF THE TEST, TO BE PERFORMED AT AN ACTEL-DESIGNATED TEST FACILITY. 3. AT EACH 500 HOUR TEST POINT, CREATE A TABLE OF TEST FAILURES, PER BURN IN BOARD (WITH BIB MAPPING WHICH SHALL SHOW WHICH DEVICES WERE ON EACH BIB), IDENTIFYING THE PARAMETERS UNDER WHICH THE SELF-TEST INDICATOR ON THE BURN-IN-BOARDS INDICATED A PART FAILURE. 4. PERFORM FULL PARAMETRIC EVALUATION ON EACH PART EVERY 1000 HOURS ON THE AUTOMATED TEST EQUIPMENT AT THE CONTRACTOR S FACILITY. LOG AND DELIVER TEST RESULTS, HIGHLIGHTING ANY PARAMETER OUT OF RANGE OF THE SPECIFICATION LIMIT. ATE TESTING SHALL BE PERFORMED AT 25C. ZERO HOUR (START) AND 6000 HOUR (FINISH) READ POINTS SHALL BE PERFORMED AT -55C, 25C, AND 125C. DELIVERABLES: THE CONTRACTOR SHALL DELIVER LOG/REPORTS OF SELF-TEST ERRORS AS INDICATED BY THE DESIGNED PINS ON THE BURN-IN-BOARDS DURING THE ENVIRONMENTAL TESTING. (TASK 3) THE CONTRACTOR SHALL PROVIDE ELECTRONIC MESSAGE PART EVALUATION SUMMARY EVERY 1000 HOURS. (TASK 4) THE CONTRACTOR SHALL DELIVER FAILURE ANALYSIS REPORT(S), IF A FAILURE OCCURS. (TASK 3 AND 4) THE CONTRACTOR SHALL DELIVER A FINAL REPORT CONTAINING ALL TEST DATA, AND A SUMMARY OF THE TOTAL TEST RESULTS, INDICATING ANY INSTANCE OF TEST DATA OUT OF SPECIFICATION LIMITS DURING THE TESTING. THE CONTRACTOR SHALL RETURN THE 160 FPGA PARTS TO NASA AFTER THE COMPLETION OF THE TESTING. DELIVERABLES ADDRESS: THE DATA DELIVERABLES SHALL BE SENT VIA EMAIL IN TEXT FORMAT TO THE FOLLOWING: COMPATIBILITY/READABILITY ISSUES SHALL BE WORKED OUT IN ADVANCE BY BOTH PARTIES (I.E., THE CONTRACTOR AND THE GOVERNMENT). MITCHELL DAVIS 301-286-4114 MITCHELL.L.DAVIS@NASA.GOV THE FPGAS SHALL BE RETURNED TO: MITCHELL DAVIS NASA GODDARD SPACE FLIGHT CENTER BUILDING 20 ROOM 180 MAILSTOP 565.0 GREENBELT, MD 20771 PERIOD OF PERFORMANCE: THE PERIOD OF PERFORMANCE OF THIS PURCHASE ORDER SHALL BE FROM RECEIPT OF THE FULLY EXECUTED PURCHASE ORDER THROUGH JUNE 30, 2009. ITEMS TO BE FURNISHED BY GOVERNMENT: 80 PARTS OF RTAX250S -CQ208 AND 80 PARTS OF RTAX2000S -LG624 ALONG WITH PROGRAMMING DATABASE FOR EACH DESIGN. (DELIVERED TO ACTEL ON APRIL 25TH, 20