MO-PR-TPD-GO-0027i3 - IUP Universität Bremen
Contents
1. a ok Section 3 7 AD5 as Set up Sun Simulator at Nadir window_ OK fF AD5 Align Sun Simulator aa ADS 109 MonironTaL KI mo suneaora fo 111 Decision to proces Jox TB2 Section 3 7 Section 3 7 nd Sun simulator at sun TB2 109 0 69 Rad Irrad in nadir mode gt D dm tas ab as Set up Rad Irrad in Nadir mode ok Align Rad Irrad Set up in Nadir mode lok ok 114 Set up Sun Simulator at Sun window O Align Sun Simulator This document contains proprietary N information of TNO All rights reserved Tke gt o1 iw SJ o OK OK OK OK OK fraurapTaL fk fseoionsz K OK OK OK OK K K gt D5 aa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 19 of 26 FM identification Calibration Step description Nominal Actual Reference Value Value ne r to Section TT 1m7 monrnon OK Seationg7 ooo S 118 OK Section 3 7 Ok E Sphere in nadir TB2 20 Install TVSPH in front of Nadir window 121 Align TVSPH with respect to GOME2 entrance slit SPHERE_TAL 23 MONITOR TAL 4 Decision to proceed 46 11 Sphere on sun port TB2 25 Install TVSPH in front of Sun window 26 Align TVSPH with respect to GOME2 sun port 4 o A o i o a i AD5 TI _ tas a Oo a N N Section 3 7 Section 32. yes hm JIN My N JO oO Start from menu bar menu gt tools gt ATP gt start DS oe ATP Og_start no parameters Og_start will now appear in ATP status window should be yellow now i e the ATP is waiting Input N and ICU on buttons on power supply gt yes push buttons EQ ON and ICU ON lift cap push button close cap do nothing if buttons are already green ICU display should read 28 00 V 0 43 A EQT display should read 28 00 V 0 00A Wait for approximately 1 minute Input Operator name use your personal first name for this gt OK Input Context_FPA_cooling_enabled y n gt n safe mode gt OK ao Be sure about yes FPA vacuum on a Input Context_PMD_cooling_enabled y n gt n safe mode gt OK Be sure about yes in vacuum only Input Context_PMD_flight_line_enabled y n gt n safe mode gt OK Input Context_QTH_high_current_enabled y n gt n 360 mA y 420 mA TBC gt OK Input Continue with BIT y n gt shall be y for each long measurement and or frequently gt OK BIT Built In Test Input Enable monitoring y n gt y gt OK Input ATP Get_packet in ATP status window From the options 1 RTR 2 RT 3 RTE select option 3 i e everything verify set values in the DAPB start up window Station type DAPB 1 Instrument model FM1 1 2 or
3. 198 Pack GOME2 instrument EGSE and other equipment 199 Post Test Review PTR O OK ie This document contains proprietary N information of TNO All rights reserved Tke Aaa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 22 of 26 4 10 Non conformance Reporting In failure cases non conformance reporting shall follow prescriptions of the Product Assurance Plan 4 11 Deviations from the Procedure Deviations are acceptable as long as test purposes and objectives remain valid In any case deviations need to be introduced via the Procedure Variation Sheet A form sheet is provided in section 6 Where a non conformance was the reason for a procedure deviation a non conformance report needs to be generated separately This document contains proprietary information of TNO All rights reserved Tke Aaa a a a a a T P D Space Instrumentation BONS SD RITRO DATE 16 August 2002 PAGE 23 0f 26 5 Procedure sign off sheet The identified test article has been successfully calibrated in accordance with this procedure and all open items and non conformance reports are closed except those listed here below Date and signatures of Test Manager Product Assurance Customer This document contains proprietary information of TNO All rights reserved Tke aa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DA
4. DATE 16 August 2002 PAGE 6 of 26 Gomez2 handling transportation and installation procedure MO PR TPD GO 0025 latest issue Gome2 emergency procedure for the VCF MO PR TPD GO 0029 latest issue Optical and mechanical alignment procedure OPR020003 List of applicable Gome2 FMx instrument NCR s To be provided by GAL ATP report MO RP TPD GO 0037 latest issue TVC user manual Gome2 safety guideline for Calibration MO NT GAL GO 0025 latest issue Reference documents Acronyms Acronym Description AIRR Ambient Irradiance Radiance set up ATP Automated Test Procedure BEPNT ODBH Bus Probe New Technology CTB Command and Telemetry Block DAPB Data Acquisition and Processing Block EGSE Electrical Ground Support Equipment ESA European Space Agency FMUSIM Fast Multiplexer Unit Simulator FPA Focal Plane Assembly GAL Galileo Avionica Gome Global Ozone Monitoring Experiment GSE Ground Support Equipment HCL Hollow Cathode Lamp LRS Low Radiance Stimulus MGSE Mechanical Ground Support Equipment NCR Non Conformance Report OGSE Optical Ground Support Equipment This document contains proprietary information of TNO TPD All rights reserved TRO ae a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 7 0f 26 Acronym Description PMD Polarisation Measurement Device PVS Procedure Variation Sheet QTH Quartz Tungsten Hydrogen Lamp SMU Scan Mirror Unit SLS Spectral
5. 7 OK OK OK OK Ro sie AD5 sz mis nl Section 3 7 a Section 3 7 O S 27 SPHERE TAL 128 MONITOR TAL 129 Decision to proceed O 4 7 TVC Gome TB1 nominal 10 temp campaign 130 Switch off PMD cooling Ol i K 1 Change TB temperature and stabilise OK 32 Install LRS OK i K K OK OK OK OK Including SLS over diffuser K During 10 campaign no PMD cooling is allowed a ju wo Bl 33 Optical pre alignment of LRS with O respect to GOME2 entrance slit 134 Optical alignment check fine tuning of LRS with respect to GOME2 entrance slit 471 LRS in white light mode TB1 35 Ok 5 Ok i OK OK a ju wo E Section 3 7 Section 3 7 Section 3 7 Eta Zeta only a 37 BREWSTERSCANTAL with Xe 38 MONITOR TAL 47 2 Oriel stimulus TB1 ao 9 Set up Oriel Monochromator 40 ORIEL TAL 41 MONITOR TAL This document contains proprietary information of TNO All rights reserved Section 3 7 Section 3 7 OK OK OK BA iy Aaa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 83 DATE 16 August 2002 PAGE 20 of 26 FM identification Calibration Step description Nominal Actual Reference Value Value 47 HCL stimulus TB1 42 Set up HCL stimulus O 3 HCL TAL o 44 MONITOR TAL o 145 Decision to proceed O 474 Rad Irrad in sun mode TB1 and Sun simul
6. Light Source TBC TBD To Be Confirmed To Be Determined TVC Thermal Vacuum Chamber VCF Vacuum Calibration Facility WLS White Light Source Xe Xenon Lamp This document contains proprietary information of TNO TPD j ly All rights reserved P U ae a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 3 3 1 AD3 3 2 AD4 3 3 AD5 3 4 AD8 3 5 3 5 1 ISSUE 3 DATE 16 August 2002 PAGE 8of26 Supporting procedures applicable during Calibration Execution Operation and Handling Procedure Gome2 handling transportation and installation procedure MO PR TPD GO 0025 latest issue Emergency Procedure Gome2 emergency procedure for the VCF MO PR TPD GO 0029 latest issue Alignment Procedure Stimuli and MGSE Optical and mechanical alignment procedure OPR020003 Operation of TVC TVC user manual Switch on off procedure for Gome2 GAL ATP s Switch on procedure for Gome 2 step description o O 1 2 3 4 5 turn 19 rack on lp turn safety button at the bottom of the rack to the right ls turn on switch that is located directly above the safety button should be directed upwards now set red switch to OFF 0 i turn red switch to ON 1 boot up the BEPNT 5 push the power button on the rightmost PC located under the desk login as administrator password bent double click icon start_bep bat double click icon BEP MMI lo wait for red indicators
7. block 2 This document contains proprietary N information of TNO All rights reserved Tk e a a a a TPD Space Instrumentation oe Ci GG 00e7 DATE 16 August 2002 PAGE 16 of 26 FM identification Calibration Step description Nominal Actual Reference aa ae a 29 ShutdownGOME2 down GOME2 Install GOME2 on AIRR MGSE fst comencomestocta fox Ta 32 Connect FPA vacuum pump ok m Section 5 3 5 E a ie For on o o o o a ae on o o o o 2 enema fox fy a smenoncovse fx Sectons5 Set detector temperature at TD1 and Section 3 6 PMD must be OFF stabilise Perform functional test o Jaw Mechanical alignment of AIRR MGSE oe ADS o nee 38 Sun simuiatorin sunambient Jos y 2_finetssintomateeves f fe Mechanical alignment of SS jo AD5 Optical alignment SS with respect to AD5 GOME2 sun a e amma ft Section o e e a a a 44 Decision toproceed dx d Install GOME2 in TVC 45 shutdowncomez OK fseonss a AD1 4s RemoveGomertommese fox 47 instal Gome onTvewese fox as instalGomezintve fox 49 Connectgome2 Jx 50 _ connect FPA vacuum pump Jos Taa lee I ney 52 swichongomes fox Section 3 5 153 Pertormtunctionaltest fox tay 54 Mechanical aignmentotmese fox mos 55 _ instan LRS at Nadir window fox tas se obese Te door fox f fay 57 _ Checkwaring alarm system fox S
8. shutdown FMUSIM computer power switch under desk shutdown BEPNT close BEPNT application menu gt file gt exit shutdown BEPNT computer power switch under desk 3 6 Gome2 console This feature comprises initialisation de initialisation commands for Gome2 such as FPA PMD coolers on off set SMU angle etc The following procedure settings are applicable TBC 1 Start Gome2_console atp see section 3 7 2 Enter SMU angle 4 3 Enter code for This document contains proprietary information of TNO TPD All rights reserved TR ae a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 3 DATE 16 August 2002 PAGE 11 0f 26 200 Gome2 LED FPA off 201 Gome2 LED FPA on 300 Gome2 LED PMD off 301 Gome2 LED PMD on 400 Gomez SLS off 401 Gome2 SLS on 500 Gome2 WLS off 501 Gome2 WLS on 600 Gomez2 FPA cooler off 601 Gomez2 FPA cooler cold 602 Gomez2 FPA cooler disable 603 Gomez2 FPA cooler enable 699 Set target temperature FPA K 700 Gome2 PMD cooler off 701 Gome2 PMD cooler cold 702 Gome2 PMD cooler disable 703 Gome2 PMD cooler enable 704 Gome2 PMD cooler line 1 ground do not use 705 Gome2 PMD cooler line 2 in flight 800 Set integration time closest to Gome2 values is chosen for FPA PMD 900 Close Gome2 Shutter sun port 901 Open Gomez Shutter 902 Shutter Gome2 disable 903 Shutter Gome2 enable 998 Gome 2 in stand by idle mode 999 End 3 7 Run
9. 3 Level INSTRUMENT This document contains proprietary information of TNO TPD a All rights reserved TKO y a j ao A A 0 gt ae a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 10 of 26 sep faesonpnon Company User EZ Session description short description of measurement this description will appear in data file name ooo The subsystems are now ready for running calibration ATPs 3 5 2 Change_context tal An GAL ATP for switching on off FPA and PMD coolers Use preferably the console tal 3 5 3 History_decoder tal An GAL ATP for resetting the history decoder This ATP is used for monitoring anomalies This ATP shall be frequently executed at least after each ATP 3 5 4 Switch off procedure for Gome 2 step description o O shutdown ce Fae start ATP OG_stop menu bar menu gt tools gt ATP gt start 2 __ watfor al ATP be sopped_ o set CTB to local mode menu gt modes gt local ae exit CTB application menu gt file gt exit 5 shutdown CTB computer power switch underthe desk turnoff to raek S O e setred switch to OFF 0 o O fe turnbigred safety buttontothelett o O shutdown musim S y O soo stop FMUSIM core menu gt core gt stop FMUSIM core OK close FMUSIM application menu gt file gt close program
10. E DURING CALIBRATION EXECUTION s eessossossossooscoseseesesssossoesoeseoe 8 3 1 OPERATION AND HANDLING PROCEDURE csccscsssssssssessessessesscescessessessesecescescesesacsaecaesaesasessesessescseeseeseesessessesscsecseenaeas 8 3 2 EMERGENCY PROCEDURE saaran R E E sod gan I eae ste BAST SSCS N E Sasa e wad SR abo 8 3 3 ALIGNMENT PROCEDURE STIMULI AND MGSE ccccccsssssssssescescessessessceecescesesaesaecsecaessssaseaessesecseesesseeseaseasesscaecsecnaeea 8 3 4 OPERATION OF TVG iurare veria ra SEA EEEE A S tec tamesutuuscusink sa tenses Webeustiuas deveksstauis abet oardact neeieeee ieee 3 5 SWITCH ON OFF PROCEDURE FOR GOME2 GAL ATP S 3 3 1 SwitChsOn Procedure fOr Come 2 wisi teesicssseiessdevecassssseassadentaadeatye iesevis oxtasa sane tada sous taste addons seas asada aces ease abe abies 3 5 2 Change lt CONtext tal visecses cio sess Misc cease alls deen A A Wo see esha SE A Ah 30 3 HIStory sd C OD Ort p RE EERE Te Saw hae EEEE acti chase ca abeae casein a R 3 34 Switch off procedure fOr GOME 2 sececscecsvevsssveacianssscuvancevaansiestassunoseadhcaiaveiieacisestactaswerubaaeadsaneandisaseseabeseeaaetulevea nase 3 6 GOMEZ CONSOLE Zespri nar a a a E E A TEE E EAEE E E aE a e 10 3 7 IRWINNING ARES S E TE E 11 3 8 OGGING E ATE A E E A E A E AAE 12 3 9 BACK UP OF DAPB DA TA iickoccd cidevecenccseceecadcscescesceducas ERANA T RE E E EE RA 12 B10 QUICK LOOK e a a E R E R E E Re E 13 A STEP BY STEP PROCEDURE ssscscscsssasse
11. T P D Space Instrumentation EAO x AER DATE 16 August 2002 PAGE 1 of 26 Title GOME2 calibration Calibration execution procedures Prepared by L van Riel Checked by M Eschen 4 b r Verified by J Hopman ype 2002 00 1g Authorised by G Otter Am 2062 wf 2 This document contains proprietary information of TNO TPD Re All aghts reserved ext j ae R a a a a T P D Space Instrumentation o E E eos DATE 16 August 2002 PAGE 20f26 DISTRIBUTION LIST ome Tom m oe 1x R Veratti P Calibration Execution Team B Ricciarelli E ESA A Lef bvre J Callies DOCUMENT CHANGE RECORD Number of Short description Pages pages 20 September 2000 All 11 March 2002 Newdocument Al FM1 update ALL This document contains proprietary information of TNO TPD j ly All rights reserved P aa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 3 DATE 16 August 2002 PAGE 3o0f26 Table of Contents Ds SCOP Bizcccdicseccaceccscaace ses AE EASE IE PE ENE SE AEAEE S E E AEAEE E 5 2 DOCUMENTS AND ACRONYMS iisssscscscssecsteusuasscosesscctesonsasisudasscnenssntednsuswsesssascebesessustbebsscessasescsoesessndosedashcbsnduchssdasetebessenedeoss 6 2 1 APPLICABLE DOCUMENTS 2 2 IREFERENGE DOCUMENTS Sinani cccstcacesscax easel EE E NEEE E EE ENE OEE a ea eo esc 2 3 ACRONYM Serre an ee AE ENAN EEEE s a HEBBEN TEE NAAR EES a E e 6 3 SUPPORTING PROCEDURES APPLICABL
12. TB2 83 SetupLRSinsitmode Jx o o ooo o S 84 Fov TaLwinxe Jox Seationg7 ooo S je Fov rawha Jox seins S jee wonrrontaL kK sewon CT y This document contains proprietary information of TNO All rights reserved Tk Aaa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 18 of 26 FM identification Calibration Step description Nominal Actual Reference Value Value 46 4 LRS in monochromator mode TB2 Set up LRS in monochromator mode ok MONOSCAN TAL lok lok MONITOR TAL o aed Section 3 7 For straylight 90 _ Decision to proceed Ol Section 3 7 65 HCL stimulus TB2 Set up HCL stimulus loK O 92 HCL TAL ox 93 MONITOR TAL 66 ORIEL stimulus TB2 K OK OK K OK K OK Set up Oriel stimulus OK OK OK K OK OK K K Section 3 7 For FPA wavelength Section 3 7 calibration Section 3 7 For PMD wavelength Section 3 7 AD5 ADS calibration o 95 ORIEL TAL l j96 MonirontaL Jx 6 7 Zenith sky measurement 98 _ Optical alignment of Zenith Sky setup OK 99 _ ZENITH ox s TB gt N ZENITH TAL 100 MONITOR TAL Section 3 7 101 Decision to proceed 468 Rad Irrad in sun mode TB2 and Sun simulator at nadir TB2 instal Rad rrad Setup OK Setup Radiradin Sunmode ok Align Radlirad Setup in Sun mode OK instal Sun simuiator fox
13. TE 16 August 2002 PAGE 24 of 26 Procedure Variation Sheet 6 Procedure No TNO TPD Procedure Variation Sheet Date Issue Sheet Project Project Gome 2 Instrument Calibration 2 Instrument Calibration PVS No Cal Test Step description Nominal Value Actual Value au Remarks ae Test Operator Customer Location This document contains proprietary information of TNO TPD a All rights reserved THe aati Aaa R a a a a T P D Space Instrumentation So TE DATE 16 August 2002 PAGE 25 0f 26 7 Gome 2 NCR s affecting Calibration Execution GAL info The following pages reflect the GAL raised NCR s which should be taken into account during calibration The following pages are incorporated as is with references FM1 e mail from GAL B Ricciarelli dated 8 march 2002 This document contains proprietary information of TNO TPD All rights reserved Ep wy ae a a a a TPD Space Instrumentation This document contains proprietary information of TNO TPD All rights reserved TRO DOC NO ISSUE DATE PAGE MO PR TPD GO 0027 3 16 August 2002 26 of 26
14. TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 21 of 26 FM identification Calibration Step description Nominal Actual Reference Value Value 71 MONITOR TAL lok Section 7 4 8 2 HCL stimulus Section 3 7 Section 3 7 175 Decision to proceed PF 3 Oriel stimulus TB3 Biz N 2 3 4 Set up HCL stimulus TB3 HCL TAL MONITOR TAL e A N e A Az LA gt fen A Set up oriel Monochromator all o A A 77 ORIEL TAL Section 3 7 178 MONITOR TAL Section 3 7 48 4 Rad Irrad in sun mode TB3 and Sun simulator at nadir TB3 179 instal Raamaa setup Jox fms 180 Set upRadiiradinsunmode ok mos 181 Align Radlirad Set upinsunmode fox fans 182 instali Sun simulator fox ADS 183 Set up Sun Simulator at Nadir window ok mos 184 Aion Sun simulator ok f fms MONITOR TAL SUNRAD TAL 48 5 Rad Irrad in nadir mode TB3 and Sun simulator at sun TB3 A iw o 188 Set up Rad Irrad in Nadir mode 9 li 0 O A 11a oe OK OK Align Rad Irrad Setup in Nadir mode Set up Sun Simulator at Sun window 1 2 3 4 Align Sun Simulator FELIRR TAL MONITOR TAL SUNIRRTAL 195 Decision to proceed Post test and packing gt a fa a fafa o e So O A A oO Az A o O A Section 3 5 AD1 p gt o ie A 96 Perform functional test 97 Shut down GOME2
15. ator at nadir TB1 146 ox ma 147 Setup Ra madinSunmode fox mos 148 Align Radiirad SetupinSunmode fok mos 149 instal Sun Simuiator fox fms 150 Setup Sun Simulator at Nadir window OK mos 151 Align Sun Simuiator fox faos jis F asstat do Seationg7 ooo S 153 wonrontaL Jo fse ionss oo 154 susia o doa Seationg7 d 4 7 5 Rad irrad in nadir mode TB1 and Sun simulator at sun TB1 155 Setup Radiirad in Nadirmode fox tangy J o ooo S 156 Align Radnraa Setupinnadrmode ox fes ooo 157 Setup Sun Simulator atsun window ok fas o ooo S 158 Align sunsimuiator fo fes o isa F aBsara Jo Ssenari S monrnon fox Seton TT Jsusra ooo do d o Sectona C a 4 8 TVC Gome TB3 nominal 10 temp campaign 3 ow a 64 O a ee 65 finial RS ssid LRS OK e EO i ote e r respect to GOME2 entrance slit Optical alignment check fine tuning OK AD5 of LRS with respect to GOME2 entrance slit 481 LRS in white light mode TB1 O o ee ee sectiona7 ewzeaony ie Psedions o di Section 3 7 Section 3 7 en K K a ae a uo o O N ee a fafa fi D Q O 8 Set up LRS in White light mode OK 169 BREWSTERSCANTAL with QTH OK 170 BREWSTERSCANTAL with Xe OK This document contains proprietary information of TNO All rights reserved iy aa a a a a a TPD Space Instrumentation DOC NO MO PR
16. c Log predefined format 3 Measurement Log tracking of measurements i e ATP s excerpt of the electronic log Parameters to be frequently monitored and to be logged parameter Z Z vawe _ remak ee y O Instrument WLS current Typica36eoma SSS O Instrument temperature FPA s PMD s Tref Tref Pre disperser Prism Temperature TVC cold finger temperature lt ms S O FPA vacuum pump pressure lt 10 mbar Heater Cooke temperate __ _Typieal fd History decoder E the end of each ATP or more frequently when necessary w r t file size Built In test ST AL OG start _ re ee D ey 3 9 Back up of DAPB data The DAPB raw data i e the archived measurements shall be frequently archived back up on CD ROM identified with e Source including Gome2 FMx e Date Time e Made by This document contains proprietary information of TNO TPD All rights reserved TR ae a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE eS DATE 16 August 2002 PAGE 13 of 26 The obtained back up shall be indicated in the logbook 3 10 Quick Look Quick look analysis shall be carried out e Inspection of DAPB Science Panels before execution of an ATP by dry run of the ATP e Inspection of DAPB Science Panels during ATP run e Using conversion tool off line after execution of ATP The parameters to be monitored for quick look analysis e General insight befo
17. cssssosoussossstdesssseecedsasactsons sse reo Pi EN S Siosar ont oeo haro DESE S ROES iai ToS ODES SOES 14 4 1 GENERA WD ne er ee 14 42 PREPARATIONS eieae eae ECE APESE ERE Sevecetecduvvtsesbuccudsuecseccansestsesecisesseusussuesuedeeeteeduete tevsssussedaievateuscsecegecusecusntesetvesecs 15 4 3 AMBIENT BLOGK di R E A E E E E E E 15 4 4 AMBIENT BLOCK Zaren a e a E E E AAE E A A A E EA E E 15 4 5 INSTA E GOMEZ N TVG a wa aE ed AATA A 16 4 6 TVC GOME TB2 NOMINAL TEMP CAMPAIGN sccsscsssssessesscsscescessscssecescesceseesssecsecsecaacsacsacseeseeseseaseaesseseeseeeessesenas 16 4 6 1 LRS in White light mode 4 6 2 LRS in filter mode TB2 46 3 LRS in slit mode TBZ Jerne tate scab acento a oD cae Rite gases te ees ea dagen Rae 4 6 4 LRS in monochromator mode TB2 scscscsscscssssvsesssessesseesessscscesessssssesessssssessassessesssesessessussecseseasseeseseeseeseaeeesaeseseeeees 18 4 6 3 HCE stim lus 1 B2 senene a a a a a a r S 18 466 ORIEL stimulus T B 2 e a a a aaa iv eestietiisiea 18 4 6 7 Zenith sky measurements TB2 cccccccesesscsesesevsesesssessesssesesescesesessesesesesssssseseaseesessseeeseseseeecseseaseeeseseeeeeeseseeenseseeeeees 18 4 6 8 Rad Irrad in sun mode TB2 and Sun simulator at nadir TB2 eccccccccsccsssssscsesssseseseseseesssesessseseesessssssesesseeees 18 4 6 9 Rad Irrad in nadir mode TB2 and Sun simulator at sun TB2 c cccccccscsccssssssssessssesesesessesssesesessseseessesesesseees 18 4 6 10 Sphere innadi
18. e ef respect to GOME2 entrance slit 59 SwitchGomezof Gomez off lok sections Sf Gome 2 to vacuum gt 10 AD8 aa ei Start of Bake out oc Jag D8 TVC Gome TB2 nominal temp campaign This document contains proprietary information of TNO All rights reserved Aaa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 17 of 26 FM identification Calibration Step description Nominal Actual Reference 4 4 fan emeas a ll E A has decreased below 303 K te ee stabilise idl sacl i BE ose acc stabilisation on a S results EA LRS alignment Jaa O Optical alignment check fine tuning AD5 of LRS with respect to GOME2 entrance slit 46 1 LRS in White light mode Change detector temperature to TD2 Section 3 6 ea 1 stabilise 70 LINEARITY TAL O O TAL Sections7 3 7 MONITOR TAL s Section 3 7 Change detector temperature to TD1 Section 3 6 and stabilise Section 7 a eS S 75 orruserMonta fox Sectons7 itfuser monitoring 76 _ BREWSTERSCANTALwih TH ok Seoionsz moudeserazera 77 BREwstenscantaL with xe ox Seating 78 wonronTaL OK Section 7 moudeserazera 46 2 LRS in filter mode TB2 72 _ event nade _fo__ __ ___ ___ _ __ FILTERSCANTAL with Xe Section 3 7 Dispersion and cross Sa a jet FLTERSCANTALwithaTH ox Section 3 7 eee ee 46 3 LRS in slit mode
19. in the application window to become green check all acquiring panel checkboxes to ON 10 fF boot up FMUSIM 12 13 14 11 push the power button on the leftmost PC located under the desk login as administrator password bent lig o double click icon FMU SIM MMI ignore error message FMU SIM Core not present gt OK Start from menu bar menu gt core gt start FMUSIM you have to click OK twice Start from menu bar menu gt core gt connect to FMUSIM in the application window section panel subsection input click nominal 2 in the application window section panel subsection output click nominal 1 This document contains proprietary information of TNO TPD N All righ rights reserved P aa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 3 DATE 16 August 2002 PAGE 9 of 26 see fasoron aaa in the application window section panel subsection commands click generation on in the application window section panel subsection commands click acquisition on in the application window section panel subsection commands click distribute on check 19 rack 21 alnumbersinthe digital displays should beclosetozero SS O boot up CTB user TPD_sidney worn dir TPD_FM1 Start from menu bar menu gt modes gt online gt
20. ins proprietary information of TNO All rights reserved Tke Aaa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 15 of 26 FM identification Calibration Step description Nominal Actual Reference Value Value 4 2 preparations Arrival of GOME2 EGSE and other ieee ness dae enone EGSE and other equipment 3 incoming inspection inspection ao CTB DAPB Pump Cooler lal A E E Y EGSE systems Install router logiPadressss sid IP adresses 7 _ Connect OAC to EGSE sub network aAa e e a Checknetworkperiormance fo o o i y S arwaotaomeerm Jx 10 Unpackaomer fox o awn S S m inspectaomer o dos o o S 12 Acceptance review OK Document in acceptance report 4 3 Ambient block 1 13 nsancomezonaeramose fos ray 14 Connectgomeztocta fox fram S 15 Connect FPA vacuum pump fox fay S 16 Connect Radiant Cooler fox lew S 17 switehongomez fox Sections df 18 Set detector temperature at TD1 and OK Section 3 6 PMD cooling must be OFF stabilise L19 Performfunctionaltest fox tty S l 20 Mechanical alignmentoraeTamase lox aos 21 install LRS in frontofGome2 nadir ok laos l 22 setupLRSinwntetignmoe Jos e E a to GOME2 entrance slit joa monrorra fox Section l as aeram O fo o fse O Sectons7 ox renee ee a o 8 Decisiontoproceed doa Ambient
21. ning ATP s For information concerning ATP s i e structure settings etc reference is made to AD7 Start from CTB menu bar menu gt tools gt ATP gt start select ATP enter Y click OK List of applicable ATP s For information only aterm oese mese vn mwm m AETA tal LRS AETA NADIR ambient TD1 AIRR tal SunSim AIRR SUN ambient TD1 BREWSTERSCAN tal LRS TVC NADIR TB123 TD1 FILTERSCAN tal LRS TVC NADIR TB2 TD1 IFOV tal LRS TVC NADIR TB2 TD1 FELRAD tal FEL TVC NADIR TB123 TD1 FELIRR tal FEL TVC SUN TB123 TD1 This document contains proprietary information of TNO TPD N j ly All rights reserved P U ae a a a a a T P D Space Instrumentation St See DATE 16 August 2002 PAGE 12 of 26 aterm oese mese vn mwm m SUNRAL tal SunSim TVC NADIR TB123 TD1 SUNIRR tal SunSim TVC SUN TB123 TD1 LINEARITY tal INT LED TVC NA TB2 TD12 MONITOR TAL INT LED TVC AETA AIRR NA TB123 TD12 MONITOR TAL INT WLS TVC AETA AIRR NA TB123 TD12 MONITOR TAL INT SLS TVC AETA AIRR NA TB123 TD12 DIFFUSERMON TAL INT SLS TVC NA TB2 TD1 ORIEL tal LRS TVC NADIR TB123 TD1 MONOSCAN tal LRS NA NADIR TB2 TD1 HCL tal SLS RAD TVC NADIR TB123 TD1 SPHERE tal SPHERE IRR TVC SUN TB2 TD1 SPHERE tal SPHERE RAD TVC NADIR TB2 TD1 ZENITH tal ZENITH TVC NADIR TB2 TD1 3 8 Logging Logging shall be applicable during the calibration campaign The following log forms shall be used 1 Hand written Log free format 2 Electroni
22. r TB2 erreen E E E E ec hese E R E E R 19 This document contains proprietary information of TNO TPD a All rights reserved TKO Li Aaa R a a a a I P D Space Instrumentation E E cc DATE 16 August 2002 PAGE 40f26 4 6 11 Sphere ON SUM POTE D I castes sreichajecteassiaiasandasahestausah tavauia EE OE R sete 47 TVC GOME TB1 NOMINAL 10 TEMP CAMPAIGN 4 7 1 LERS in white light mode TB s ccccccccsccccdescssacsecsnssnthatecceecastecese deci eies sas dhaveadeiciechslieieeeiiesecdladsesseatilascns teecietactesse ose 4 7 2 Oriel stimulus TB1 4 7 3 HCL stimulus TB1 4 7 4 Rad Irrad in sun mode TB1 and Sun simulator at nadir TB1 4 7 5 Rad Irrad in nadir mode TB1 and Sun simulator at sun TB1 48 TVC GOME TB3 NOMINAL 10 TEMP CAMPAIGN ccccscsssssssscescessessseecescscseeseesecsecsecsscsacsacseeseeeseaseasseesecseeeeesesenss 4 8 1 ERS in white light mode TBI iccccceccecsceseieis cassestecindessecctsctshteesddelvsatees O REE EEN EEE RAE ESR AiB2D gt HCE stim luS sseni sivas Ree Bs En RE AES 21 4 8 3 Oriel stimulus TBI areren aE fos bis esas ial E BAT BLE EE on cURL REEL 21 4 8 4 Rad Irrad in sun mode TB3 and Sun simulator at nadir TB3 c cccccccccsccsessescsesessesesesesensscesessseesesessessaeseesees 21 4 8 5 Rad Irrad in nadir mode TB3 and Sun simulator at SUN TB3 cccccccscccsccsssssscsesesseseseseseesscesessesseesesseesseseeseeess 21 49 POST TEST AND PACKING ccccccsscssscssssssecssssssec
23. re during after ATP execution e Signal to noise ratio e Saturation lt 50000 counts typical 40000 e Signal gt 10000 counts e Instrument condition temperatures environment etc Before a set up change ambient to vacuum OGSE change etc a successful executed ATP is required This document contains proprietary information of TNO TPD j ly All rights reserved P U Aaa a a a a a TPD Space Instrumentation DOC NO MO PR TPD GO 0027 ISSUE 38 DATE 16 August 2002 PAGE 14 of 26 4 Step by step procedure 4 1 General The following shall be taken into account prior and during Calibration Execution not in order of importance Check Operation and Handling Procedure AD1 shall be present Emergency Procedure AD4 shall be present Gome2 safety Procedure AD9 shall be present Alignment Procedure AD5 shall be present Stand by operator for TVC and VCF shall be arranged SMS service for TVC alarm warnings assigned Implications of GAL NCR s checked section 7 Gome 2 automatic shut off system for TVC pressure installed and tested Never use PMD coolers ON during ambient conditions and during 5 C calibration QCM software installed for monitoring Coffee Machine shall be present and working Log sheets shall be present JU UQUUHUUE It shall be noted that the following step by step procedure wr r t the sequence is not mandatory Measurements order may be changed when convenient This document conta
24. scesssececesssecesessssesesuesseseacesseseacesssceecessecsesesuecseseaeecssseatecssceutecseceesecseceeees 4 10 NON CONFORMANCE REPORTING 4 11 DEVIATIONS FROM THE PROCEDURE 5 PROCEDURE SIGN OFF S HEET 0 sccccssssscsssscecsssssscecessscssscssessssecessssecssssscesesscnssssscessesesssessesesesscsesesscsasecesscsesesesessecesers 23 6 PROCEDURE VARIATION SHEE T scssscssssssssssssssssssssssssssssssssecsssssscssessscesessssssssesessesessseasesesessecesssscsssesessesesesesessesesers 24 7 GOME2NCR S AFFECTING CALIBRATION EXECUTION GAL INFO cscscsscsssssssssesesscsssssecsssssesessesesesecsesesers 25 This document contains proprietary information of TNO TPD All rights reserved TXO Aaa R a a a a TPD Space Instrumentation Doo street DATE 16 August 2002 PAGE 5of26 1 Scope This document presents the calibration execution procedure including the step by step procedure to be applied for the calibration of the Gome2 instrument This procedure is applicable for Gome2 FM1 FM2 and FM3 This document contains proprietary information of TNO TPD All rights reserved P U TPD 2 2 1 AD1 AD2 AD3 AD4 AD5 AD6 AD7 AD8 AD9 2 2 None 2 3 AA a a a a Space Instrumentation Documents and Acronyms Applicable documents Gome2 Calibration Requirements Specification MO RS GAL GO 0003 Gome2 Calibration Plan MO PL TPD GO 0004 a DOC NO MO PR TPD GO 0027 ISSUE 3
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