1 Pre EVA Configuration3 EGRESS4 ---->EV1 Egress Airlock5 ---->EV1 Recieve and Stow Strut Bag 2 on A/ HR6 ---->EV1 Recieve and Stow Strut Bag 1 on BRT7 ---->EV2 Egress Airlock and Stow Strut Bag 2 on BRT8 ---->EV2 Translate to P1 Bay 129 ---->EV2 Attach Anchor Hooks (EV1->HR 3652 EV2->HR 3651)10 WORK SITE PREP11 ---->EV2 Translate to and Attach GREEN hook to 2B P6 HR 530912 ---->EV1 Translate to P5 HR 520313 ---->EV1 Translate zenith to and Attach GREEN hook to 4B P6 HR 531114 ---->EV1 Translate to and Stow Strut Bag on P6 HRs 5350-536015 ---->EV2 Translate to 2B lEA and Stow Strut Bag on P6 HRs 5305-530716 ---->EV2 Open Strut Bag 2 and secure lid then as time permits translate to and do Strut Bag 117 ---->EV1 Translate to port CETA Cart WIF 0218 ---->EV1 Retrieve WIFEX w/ APFR and stow on BRT19 ---->EV1 Translate to 2B lEA20 ---->EV1 Install WIFEX n WIF 38 [6,G,5]21 2B UPPER BRACKET BUILD22 ---->EV1 Translate to EV223 ---->Retrieve and Assemble Right Upper Strut L7 to Mounting Bracket L7 using PGT [B3, CW2]24 ---->Retrieve and Assemble Left Upper Strut to Center Pad using PGT [B1, CW2]25 ---->Assemble Left Upper Struts to Mounting Bracket using PGT [B3, CW2]26 ---->EV2 Torque Right Upper Struts to Mounting Bracket using PGT [B3,CW2]27 ---->EV2 Move PGT w 7116 to Right Upper Strut HR28 2B CENTER PAD TO MAST CANISTER29 ---->EV1 Translate to and Ingress APFR30 ---->EV2 Transfer Mounting Bracket Assembly w/PGT to EV131 ---->EV2 Stow PGT w 5/8 socket on HR 537232 ---->EV1 Install center Pad to mast canister using PGT [A2, CW2]33 ---->EV1 InstallNerify grounding Pip Pins into grounding block and close MLI34 INSTALL 2B LEFT STRUTS35 ->Left Lower Strut Install36 ---->EV1 Retrieve PGT w 7116 Wobble then Egress APFR37 ---->EV1 Transfer PGT to EV2 then adjust WIFEX to [6,G,1]38 ---->EV1 Adjust APFR to [12,NN,G,12]39 ---->EV1 Receive Left Mid Strut from EV2 and stow on BRT40 ---->EV1 Ingress APFR41 ---->EV1 Receieve Left Lower Strut from EV242 ---->EV2 Translate to SAAB launch bracket and Verify bearing alignment43 ---->EV2 Install Left Lower Strut M21 to SAAB bracket using PGT [A1,CW1] 4 turns only44 ---->EV1 Install Left Lower Strut L5 to Mounting Bracket L5 using PGT [B1, CW2] on Bolt M2245 ---->EV2 Drive M21 to torque using PGT [B7,CW2]46 ---->EV2 Use PGT in Ratchet to set torque on M21 PGT [Mech, RCW, 30,5] 5/8 x 2 Socket47 ---->EV2 Stow PGT on HR 5372 and Verify MLI in place48 ---->EV1 Stow PGT and Install grounding PIP pin to grounding block49 ->Left Mid Strut Install50 ---->EV2 Translate to mast canister Left Pad Install location51 ---->EV1 Retrieve Left Mid Strut from BRT52 ---->EV1 Release PIP Pins and Extend Side Pad to EV253 ---->EV2 Install Left Side Pad to Mast Cansiter using PGT [A2, CW2] then stow PGT54 ---->EV1 Install Left Mid Strut to Mounting Bracket L8 using PGT [B1, CW2] then stow PGT55 ---->EV1 Install grounding PIP pin to grounding block56 INSTALL 2B RIGHT STRUTS, MLI & CLAMPS57 ->Right Lower Strut Install58 ---->EV1 Egress APFR and Roll APFR to [12,NN,D,12]59 ---->EV2 Retrieve Right Mid Strut and Transfer to EV160 ---->EV1 Stow Right Mid Strut onto BRT61 ---->EV1 Ingress APFR62 ---->EV2 Retrieve then transfer Right Lower Strut to EV163 ---->EV2 Translate to mast canister right side SABB launch bracket64 ---->EV2 Install Right Lower Strut M19 to SABB bracket using PGT [Al, CW1]65 ---->EV1 Release L6 grounding PIP Pin then drive Bolt L6 to L6 using PGT [B1, CW2]66 ---->EV2 Drive M19 [B7,CW2]67 ---->EV1 Stow PGT and Install grounding PIP Pin to grounding block68 ---->EV2 Use PGT in Ratchet to set torque on M19 [Mech, RCW, 30.5] then leave PGT on HR 537269 ->Right Mid Strut Install70 ---->EV2 Translate to mast canister Right Side Pad install location71 ---->EV1 Retrieve Right Mid Strut from BRT72 ---->EV1 Release PIP Pins and Extend Side Pad toward EV2 and install mddle grounding PIP Pin73 ---->EV2 Install Right Side Pad to mast canister using PGT [A2, CW2]74 ---->EV1 Install Right Mid Strut L7 to Mounting Bracket L7 using PGT [B1, CW2] then stow PGT75 ---->EV1 Install grounding PIP pin to grounding block76 ---->EV2 Drive Adjustment Collar bolts M25 and M26 on Right Mid Strut using PGT [B5, CW2]77 ---->EV2 Drive Adjustment Collar bolts M29 and M30 on Left Mid Strut using PGT [B5, CW2]78 ---->EV1 Egress APFR then Close MLI on Struts79 ---->EV2 Verify middle PIP Pin in final location and MLI covering side pad then Stow PGT on swing arm80 2B-4B TRANSITION80 2B-4B TRANSITION81 ---->EV1 Retrieve WIFEX+APFR then Translate to 4B [EA82 ---->EV1 Install WIFEX in WIF 37 [6,G,5] and Verify APFR [12,SS,F,12]83 ---->EV2 Retreive PGT from HR 5372 then Translate to 4B lEA84 ---->EV2 Tether PGT w/ 7116 Wobble Socket to Bag85 4B UPPER BRACKET BUILD86 ---->EV1 Translate to Strut Bag and Retrieve Right Upper Strut87 ---->EV2 Retrieve Mounting Bracket88 ---->EV1 Install Right Upper Strut L7 to Mounting Bracket L789 ---->EV2 Drive Right Upper Strut to Mounting Bracket bolts 4 turns using PGT [B3,CW2]90 ---->EV1 Retrieve Left Upper Strut and install Strut L8 to Mouting Bracket Left Side91 ---->EV2 Assemble Left Upper Strut to Center Pad using PGT [B1,CW2]92 ---->EV2 Drive Left Upper Strut to Mounting Bracket bolt (M15) 4 turns using PGT [B3,CW2]93 ---->EV2 Drive Left Upper Strut to Mounting Bracket bolts to Torque94 ---->EV2 Drive Right Upper Strut to Mounting Bracket bolts to Torque95 ---->EV2 Move PGT w/ 7116 Wobble to HR on Right Upper Strut96 4B CENTER PAD TO MAST CANISTER97 ---->EV1 Translate to and Inress APFR98 ---->EV1 Recieve Upper Triangle from EV299 ---->EV2 Stow PGT w 5/8 x 2 Socket on HR 5366100 ---->EV1 Install Center Pad to Mast Canister using PGT [A2,CW2] Then Stow PGT101 ---->EV1 Install Left Grounding PIP Pins into Grounding Block102 ---->EV1 Install MLI over Left Strut/Center Pad intefaces103 ---->EV1 Verify Right PIP Pin and MLI in place104 INSTALL 4B RIGHT LOWER STRUT105 ---->EV1 Retrieve PGT w/ 7116 Wobble then Egress APFR106 ---->EV2 Recieve PGT from EV1 and Stow on Swingarm107 ---->EV1 Adjust WIFEX to [6,G,1]108 ---->EV1 Adjust APFR to [12,NN,C,12]109 ---->EV1 Ingress APFR110 ---->EV2 Retrieve Right Lower Strut and Transfer to EV1111 ---->EV2 Translate to Mast Canister right side SABB launch bracket112 ---->EV2 Install Right Lower Strut to SABB bracket driving (M19) 4 turns using PGT [A1,CW1]113 ---->EV1 Install Right Lower Strut L6 to Mounting Bracket L6 using PGT [B1,CW2]114 ---->EV1 Stow PGT and Install grounding PIP pin to Grounding Block115 ---->EV1 Secure strut MLI116 ---->EV2 Drive bolt (M19) to torque with PGT [B7,CW2]117 ---->EV2 Use PGT in Ratchet to set torque on M19 using [Mech,RCW,30.5]118 ---->EV2 Stow PGT on HR 5366 and verify lower strut MLI119 2B-4B CLEANUP120 ---->EV1 Egress APFR121 ---->EV1 Inventory Strut Bag1 then Close and Cinch Bag 1122 ---->EV2 Retrieve PGT from HR 5366 and Stow in Strut Bag 2123 ---->EV2 Inventory Strut Bag 2 then Close and Cinch Bag 2124 ---->EV2 Stow Strut Bag 2 on BRT125 ---->Translate to and Retreive GREEN hooks (EV1->HR 5311, EV2->HR 5309)126 INGRESS127 ---->Translate back to AIL128 ---->EV2 Stow Strut Bag bundle129 ---->Ingress Airlock
0 US_EVA_IROSA_Prep_EVA_Get_Aheads Reconfig Dialog1 Complete 4B Mod Kit2 ->Right Mid Strut Install3 ---->EV2 Translate to mast canister Right Pad install location ---->EV1 Retrieve Right Mid Strrut from BRT5 ---->EV1 Release grounding PIP Pins and Extend Side Pad toward EV26 ---->EV2 Install Right Side Pad to mast canister using PGT [A2,CW2]7 ---->EV1 Install Right Mid Strut L7 to Upper Strut L7 using PGT [B1,CW2]8 ---->EV1 Install grounding PIP pin to grounding block9 ->Left Lower Strut Install10 ---->EV1 Egress and Roll APFR to [12,NN,H,12]11 ---->EV2 ON MCC GO Retrieve and Transfer Left Mid Strut to EV112 ---->EV1 Ingress APFR13 ---->EV2 Retreive and Transfer Left Lower Strut to EV114 ---->EV2 Translate to mast cansiter left side SABB bracket15 ---->EV2 Verify bearing alignment then install Left Lower Strut (M21) 4 turns to SABB bracket using PGT [A1,CW1]16 ---->EV1 Install Left Lower Struct L5 to mounting bracket L5 using PGT [B1,CW2]17 ---->EV2 Drive (M21) to torque using PGT [B7,CW2]18 ---->EV2 Configure PGT [Mech,RCW,30.5] then use PGT to set torque on (M21)19 ---->EV2 Put PGT back in MTR and stow on HR 536620 ---->EV1 Install grouding PIP pin to grounding block21 ->Left Mid Strut Install (ON MCC GO)22 ---->EV2 Translate to mast canister Left Pad Install location23 ---->EV1 Retrieve Left Mid Strut from BRT and Extend side pad to EV224 ---->EV2 Install Left Side Pad to mast canister using PGT [A2,CW2]25 ---->EV1 Install Left Mid Strut L8 to Upper Strut L8 using PGT [B1,CW2]26 ---->EV1 Install grounding PIP Pin into grounding block27 ---->EV1 Egress APFR28 ->4B Clamps & MLI (ON MCC GO)29 ---->EV2 Drive Left Mid Strut Adjustment Collar bolts (M29) and (M30) to torque using PGT [B5,CW2]30 ---->EV1 Close MLI on Left Side Struts31 ---->EV2 Drive Right Mid Strut Adjustment Collar Bolts (M26) and (M30) to torque using PGT [B5, Cw2]32 ---->EV1 Close MLI on Right Side Struts33 ->Worksite Cleanup34 ---->EV2 Retreive PGT from HR 5366 and Stow in Strut Bag 135 ---->EV2 Perform Strut Bag 1 Inventory then Close Bag36 ---->EV2 Retrieve and stow APFR on BRT37 ---->EV2 Translate to Strut Bag 2 and perform Inventory38 ---->EV1 Bundle Strut Bag 1 to WIFEX then Retreive and stow WIFEX on BRT39 ---->EV1 Translate to P6 HR 5311 to retrieve GREEN hook40 ---->EV2 Translate to P6 2B WIF 31 install APFR with Settings [12,I1,F,12]41 ---->EV2 Translate to P6 HR 5309 to Retrieve GREEN hook42 ---->EV1 Translate to port CETA Cart WIF 3 and install WIFEX with settings [4,-,1]43 P6 WIF Integrity Check44 ---->Translate to P6 4B WIF 08 then inspect WIF and report gap status to MCC-H45 ---->Install APFR into WIF 08 and Check WIF for any motion46 ---->Retreive APFR and stow on BRT47 A (P4) SABB Base Joint Restraint48 ---->Translate to 4A SABB launch restraints49 ---->Install Wire Ties50 P4 MMOD Cover Bolt Release51 ---->Translate to P4 MMOD Cover52 ---->Release Bolt 3 using PGT [B2,CCW2]53 ---->Release Bolts 4, 1, 2 using PGT [B2,CCW2]
iss064e015374 (Dec. 28, 2020) --- A pair of U.S. spacesuits are pictured inside the Quest airlock packed with a variety of hardware ahead of planned spacewalks for upgrades and maintenance outside the International Space Station.
On Sunday, Feb. 28, NASA Astronauts Kate Rubins and Victor Glover will step out of the space station to begin assembling and installing modification kits required for upcoming solar array upgrades. The current solar arrays are functioning well, but have begun to show signs of degradation, as expected, as they were designed for a 15-year service life. The first pair of solar arrays were deployed in December 2000 and have been powering the station for more than 20 years. Later this year, the new solar arrays will be positioned in front of six of the current arrays, increasing the station’s total available power from 160 kilowatts to up to 215 kilowatts. Rubins will be extravehicular crew member 1 (EV 1) wearing red stripes. Glover will be extravehicular crew member 2 (EV 2) and wear a suit with no stripes. This spacewalk will be the third of Rubins’ career. Glover has conducted two spacewalks as part of this expedition, making the spacewalk on Feb. 28 the third in his career. It will be the 235th in the history of station assembly, maintenance, and upgrades. Live coverage of the Sunday, Feb. 28, spacewalk will air on NASA Television, the NASA app, and the agency’s website at 4:30 a.m. EST, with the crew members scheduled to exit the station’s Quest airlock about 6:00 a.m. EST.
Gotta say, I’m loving the format of the top post. All the most relevant information right there. That should be the new standard.
Quote from: Jansen on 02/02/2021 05:23 pmGotta say, I’m loving the format of the top post. All the most relevant information right there. That should be the new standard.Can we add the EMU numbers there? :-)
On Wednesday, they were joined by Hopkins and Noguchi to perform “fit-checks” of their suits—with Rubins set to wear EMU No. 3015 and Glover EMU No. 3009—and later participated in a review of EVA-71 procedures with teams at Mission Control.
https://www.americaspace.com/2021/02/25/artemis-team-duo-prepare-for-sunday-morning-spacewalk/QuoteOn Wednesday, they were joined by Hopkins and Noguchi to perform “fit-checks” of their suits—with Rubins set to wear EMU No. 3015 and Glover EMU No. 3009—and later participated in a review of EVA-71 procedures with teams at Mission Control.