Progress 23P Cargo Manifest as of 11 August 2006
Line Item | System | Part Number | Part Name (Russian) |
Part Name | Qty Up | Mass (Kg) | Length (cm) | Width/Dia. (cm) | Height (cm) | Total Mass (Kg) | Total Volume (cm3) | Notes | Justification | |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
1 | ____________ ____________ | US HARDWARE | 284.21 | 900203 | ||||||||||
2 | _______________ ________-_ ________ ________ _______ _ _____ _______-_ _______ | US PROVIDED FOOD AND CREW PROVISIONS | 165.5 | 463246 | ||||||||||
3 | ___ | FOOD SUPPLY SYSTEM (___) | 132 | 313611 | “15 US food containers are for E14 and 3 for E13 FE2. Per OC management’s request, 4 food containers are added to 23P launch manifest.” | |||||||||
4 | ____________ ________ _______ | AMERICAN FOOD | 132 | 313611 | See Above | |||||||||
5 | FOOD SUPPLY | SEG48102008-301 | ____________ ______________ _______ _________ | US COLLAPSIBLE FOOD CONTAINER | 22 | 6 | 37.8 | 30.5 | 12.4 | 132 | 313611 | See Above | ||
6 | ___ | CREW PROVISIONS | 33.5 | 149635 | Crew provisions required for E14 until 25P launch on 2/07/07. These items are for the 2-person E14 crew of Lopez-Alegria and Tyurin. | |||||||||
7 | FCE | 528-21059-410-EXP14 | “_____ ___________, ________ _______” | HYGIENE RESUPPLY | 1 | 25 | 25 | 8 | 1.25 | 5000 | “HZ,R” | See Above | ||
8 | FCE | SEG33115639-302 | _______ ________ HUGGIES | HUGGIES WIPES ASSY | 32 | .43 | 25.4 | 11.4 | 4.5 | 13.8 | 31584 | “HZ,R” | See Above | |
9 | FCE | SEG33117799-301 | _______________ ________ | DISINFECTANT WIPES ASSEMBLY | 8 | .25 | 25.4 | 10.7 | 2.5 | 2 | 4761 | HZ | See Above | |
10 | FCE | 528-21059-394-EXP14 | ________/_____/_____ | SHIRTS/SHORTS/SOCKS | 1 | 2.9 | 49 | 29 | 16 | 2.9 | 22736 | RB | See Above | |
11 | FCE | 528-21059-390-EXP14 | _____-_____ | BOXERS | 1 | 4.1 | 44 | 24 | 19 | 4.1 | 20064 | RB | See Above | |
12 | FCE | 528-21059-392-EXP14 | ________ _______ | “T-SHIRTS, BLUE” | 1 | 3.65 | 51 | 25 | 12 | 3.65 | 15300 | RB | See Above | |
13 | FCE | 528-21059-386-EXP14 | “__________ _____, ______ S” | ATHLETIC SHORTS – S | 1 | 2.75 | 50 | 22 | 21 | 2.75 | 23100 | RB | See Above | |
14 | FCE | 528-21059-388-EXP14 | “__________ _____, ______ XL” | ATHLETIC SHORTS – XL | 1 | 3.05 | 42 | 43 | 15 | 3.05 | 27090 | RB | See Above | |
15 | ________ ________ ___________ ______ (HMS) _______ CHECS | CHECS HMS HARDWARE | .51 | 355 | ||||||||||
16 | CHeCS-HMS | KLSH320082-301 | ____ _______ ___ IV-______ | “BATTERY PACK, IV PUMP ASSEMBLY” | 3 | .17 | 5.1 | 4.3 | 5.4 | .51 | 355 | “BT,HZ” | “Battery packs originally planned for 19P. Not shipped because acceptance testing not complete. Two-year extension was granted on on-orbit units (for total of 10 yrs), however exact manufacture date was not found, so expiration date is now shown as 09/05. H/w needs to be replaced and 23P is the earliest that h/w can be ready. Priority 2” | |
17 | ____-__ ________ _____ ________ (EHS) _______ ______ ________ _______ (CHECS) | CHECS EHS HARDWARE | 20.44 | 58626 | ||||||||||
18 | CHeCS- EHS |
SDD46108778-301 | _________-_____________ Grab | “VALVE ASSEMBLY, GRAB SAMPLER” | 9 | .5 | 19.1 | 12.7 | 8.9 | 4.5 | 19430 | “HZ,R” | “Resupply of GSCs to conduct nominal sampling to ensure air for crew respiration onboard ISS meets accepted standards. MORD Rev B 5.3, GGR&C. Priority 2” | |
19 | CHeCS- EHS |
SJG46120020-301 | _______ ___________ ___________ _________ _______ (CSA-CP) | “RE-SUPPLY KIT, CSA-CP” | 1 | 4.26 | 24.1 | 41.9 | 10.2 | 4.26 | 10275 | “BT,HZ,R” | “The CSA-CP is required to assess the initial severity of the toxic threat to the crew after a fire & to monitor the effectiveness of the atmospheric scrubbing. The oxygen sensor in the CSA-CP has been used as a backup measuring device to the MCA oxygen determination. MORD Rev B 5.3, GGR&C Priority 2” | |
20 | CHeCS- EHS |
SJG46120021-301 | _______ _______________ ___ ___________ _________ _______ (CSA-CP) | “ACCESSORIES KIT, CSA-CP” | 1 | 2.15 | 41.9 | 24.1 | 10.2 | 2.15 | 10275 | “BT,HZ,R” | See above | |
21 | CHeCS- EHS |
WLST400137-301 | ____________ ______ (_______) ___________ _______ ____________ __________ (VOA) | AIR IN SIEVE PACK 1 ASSY | 1 | 1.7 | 13.2 | 9.1 | 19.1 | 1.7 | 1145 | HZ | “VOA provides in-situ air monitoring, as required by MORD requirement 5.3.5, the quality of the air for crew respiration shall be monitored during all phases to ascertain that it meets the standards listed in Table 5.3-1. The VOA OMI kit hardware is necessary to replace the expired consumables & return the unit to operation. (required hardware). Priority 2” | |
22 | CHeCS- EHS |
WLST400137-302 | ____________ ______ (________________) 2 | RECIRCULATION SIEVE PACK 2 ASSY | 1 | 2.57 | 34.3 | 30.5 | 10.2 | 2.57 | 11298 | HZ | See above | |
23 | CHeCS- EHS |
0611-1141 | _____ | PUMP | 4 | .47 | 6.6 | 6.4 | 17.8 | 1.88 | 1073 | “VOA provides in-situ air monitoring, as required by MORD requirement 5.3.5, the quality of the air for crew respiration shall be monitored during all phases to ascertain that it meets the st&ards listed in Table 5.3-1. The VOA OMI kit hardware is necessary to replace the expired consumables & return the unit to operation. (required hardware). Priority 2” | ||
24 | CHeCS- EHS |
0611-2049 | _______ ______ | INLET NOZZLE FILTER | 1 | .2 | 9.1 | 6.1 | 12.7 | .2 | 318 | See Above | ||
25 | CHeCS- EHS |
0611-1107 | ___________ ______ [___________ VOA] | OXYGEN SCRUBBER | 1 | 1.71 | 45.7 | 10.8 | 6.4 | 1.71 | 3159 | HZ | See Above | |
26 | CHeCS- EHS |
0611-1108 | ____________ ______ _____ ______ _____ | NITROGEN DRYER | 1 | .26 | 18.8 | 4.9 | 2.6 | .26 | 293 | HZ | See Above | |
27 | CHeCS- EHS |
0611-2056 | __________ __________ ________________ (GC) | GC COOLING FAN | 1 | .53 | 11.9 | 4.3 | 14 | .53 | 244 | See above | ||
28 | CHeCS- EHS |
0611-2054 | __________ _____ _______ | POWER BOARD FAN | 1 | .53 | 8.4 | 8.9 | 14 | .53 | 546 | “VOA provides in-situ air monitoring, as required by MORD requirement 5.3.5, the quality of the air for crew respiration shall be monitored during all phases to ascertain that it meets the st&ards listed in Table 5.3-1. The VOA OMI kit hardware is necessary to replace the expired consumables & return the unit to operation. (required hardware). Priority 2” | ||
29 | CHeCS- EHS |
WLST400142-301 | ____ ___ ___________ VOA | VOA HARD DISK | 1 | .16 | 13.2 | 3.1 | 11.4 | .16 | 572 | See Above | ||
30 | ________ ____________ ___________ ___________ (CMS) _______ CHECS | CHECS CMS HARDWARE | 3.2 | 7348 | ||||||||||
31 | CHeCS-CMS | SJG46119447-301 | “______ _ _______ _________ TVIS, _______ _ _________ _______” | ROLLER AND TREAD BELT SPARE PARTS KIT | 5 | .45 | 20.3 | 20.3 | 3.8 | 2.27 | 4248 | R | “Resupply of bearings for limited life. Based on life prediction analysis and usage rate, a new set of bearings will be required. GGR&C. Priority 2” | |
32 | CHeCS-CMS | KLST410198-604 | ____ ___________ _________ IRED | “KIT ASSEMBLY, CANISTER CORD” | 3 | .31 | 15.2 | 4.5 | 15.2 | .93 | 3101 | Canister cords provide the load path to all the crew to exercise on IRED. These 3 cord sets add to the capability to get us to February 2007. GGR&C priority 2. | ||
33 | ________ ________ ___________ ______ (HMS) _______ CHECS | CHECS HMS HARDWARE | 10.5 | 24260 | ||||||||||
34 | CHeCS-HMS | 0264-7800-10 | “0,9% _______ _______ ______, 500 __” | SODIUM CHLORIDE 0.9% 500 ML | 5 | .56 | 29 | 12.5 | 4 | 2.8 | 7250 | HZ | “Sodium Chloride goes into the HASP and ALSP to replace those items expiring 10/30/06. These items will be stowed inside the HASP and ALSP and will not impact on-orbit stowage. Remove/replace the three expired 500 ml bags in the HASP and the two expired 500 ml bags in the ALSP. Liquids must fly in controlled environment (for launch and return) as the bags cannot withstand vacuum and may explode. Life and chemistry of fluids are also affected by the environment. MORD Rev B 4.3.4.4 C, GGR&C Priority 2” | |
35 | CHeCS-HMS | 0264-7800-00 | “0,9% _______ _______ ______, 1 ____” | SODIUM CHLORIDE 0.9% 1 LITER | 7 | 1.1 | 40.5 | 12 | 5 | 7.7 | 17010 | HZ | “Sodium Chloride goes into the HASP to replace items expiring 7/30/06 and 10/30/06. These items will be stowed inside the HASP and will not impact on-orbit stowage. Remove/replace the seven expired 1L bags in the HASP. Liquids must fly in controlled environment (for launch and return) as the bags cannot withstand vacuum and may explode. Life and chemistry of fluids are also affected by the environment. MORD Rev B 4.3.4.4 C, GGR&C Priority 2” | |
36 | ____-__ ________ _____ ________ (EHS) _______ ______ ________ _______ (CHECS) | CHECS EHS HARDWARE | 5.32 | 79140 | ||||||||||
37 | CHeCS- EHS |
KLSK270355-302 | _______ __ ________ _ ___________ ______ | MEDIA SYRINGE CASE | 1 | .14 | 15.2 | 15.2 | 2.5 | .14 | 590 | “HZ,R” | “Required for minimal, nominal water microbial sampling. In-flight water quality assessment is needed to assure that water of acceptable, defined quality will be available onboard ISS. In-flight assessment of microbial contamination is necessary to prevent the crew from being exposed to contaminated water & to evaluate critical parameters that may not be stable in archival samples. Medical experts & environmental control engineers need to know the level & types of bacteria contaminating the potable water in order to prescribe an appropriate response to ensure crew safety. MORD Rev B 5.2.2.2, GGR&C. Priority 2” | |
38 | CHeCS- EHS |
SEG46119990-303 | _______ ___ ___________________ _______ ____ | MICROBIOLOGY WATER ANALYSIS KIT | 3 | .18 | 32.5 | 22.9 | 2.5 | .54 | 5582 | “HZ,R” | See Above | |
39 | CHeCS- EHS |
SEG46119987-302 | _______ ___ ______ ____ ____ | WATER SAMPLE COLLECTION KIT | 4 | .62 | 26.7 | 45.2 | 12 | 2.49 | 57879 | “HZ,R” | See Above | |
40 | CHeCS- EHS |
WLSK270385-301 | ________ _ _______ _____ | “PACKET ASSEMBLY, PETRI DISH” | 5 | .1 | 23.5 | 14.2 | 2.5 | .5 | 4244 | HZ | “Required for minimal, normal air Microbial sampl;ing. MORD Rev B5.4.1.2 GGR&C. Priority 2.” | |
41 | CHeCS- EHS |
SEM46109455-308 | _______ ___ _____ ____ _ ___________ _________ | KIT ASSEMBLY SURFACE SAMPLER | 1 | 1 | 15.4 | 17.3 | 17 | 1 | 4502 | HZ | “Required for minimal, nominal surface microbial sampling. In-flight microbial assessment is needed (1) to assure ISS air & surfaces are not excessively contaminated with harmful microbes, including bacteria & fungi; (2) to get timely results to prevent the crew from being exposed to potentially harmful microorganisms; & (3) to evaluate critical parameters that may not be stable in archival samples. Microorganisms can also degrade systems performance & contaminate air, water, food & payload experiments. In the event that elevated levels of microbes are found, medical experts & environmental control engineers need to quickly know in order to prescribe an appropriate response to ensure crew safety & system performance. MORD Rev B 5.4.1.2, GGR&C” | |
42 | CHeCS- EHS |
KLSK270206-306 | “_______ __________ _______, 0,22 __” | “ADAPTER ASSEMBLY, AIR FILTER, 0.22µm” | 8 | .04 | 11.1 | 10.9 | 3 | .36 | 2904 | R | “Required for minimal, nominal water microbial sampling. In-flight water quality assessment is needed to assure that water of acceptable, defined quality will be available onboard ISS. In-flight assessment of microbial contamination is necessary to prevent the crew from being exposed to contaminated water and to evaluate critical parameters that may not be stable in archival samples. Medical experts and environmental control engineers need to know the level and types of bacteria contaminating the potable water in order to prescribe an appropriate response to ensure crew safety. MORD Rev B 5.2.2.2, GGR&C Priority 2.” | |
43 | CHeCS- EHS |
WLSK270378-301 | _____________ _____ | INCUBATION BAG ASSY | 2 | .02 | 30.5 | 30.5 | .3 | .04 | 557 | R | See above | |
44 | CHeCS- EHS |
KLSK270288-303 | “_____ ___ ______ _______, _______” | “BAG ASSY., WASTE, LARGE, 1L” | 2 | .03 | 37.1 | 14.7 | 1.3 | .06 | 1399 | R | See Above | |
45 | CHeCS- EHS |
90-242 | _____ ___ ________ ___________________ _______ (MCD) | MCD STOWAGE BAG | 2 | .01 | 10.2 | 20.3 | 1.9 | .01 | 787 | R | “Required for minimal, nominal water microbial sampling. In-flight water quality assessment is needed to assure that water of acceptable, defined quality will be available onboard ISS. In-flight assessment of microbial contamination is necessary to prevent the crew from being exposed to contaminated water and to evaluate critical parameters that may not be stable in archival samples. Medical experts and environmental control engineers need to know the level and types of bacteria contaminating the potable water in order to prescribe an appropriate response to ensure crew safety. MORD Rev B 5.2.2.2, GGR&C Priority 2.” | |
46 | CHeCS- EHS |
90-260 | _____ ZIPLOCK (9 ______ x 15 ______) | “ZIPLOCK, 9″”x15″”” | 4 | .05 | 22.9 | 38.1 | .2 | .18 | 697 | R | See above | |
47 | ________ ________ ___________ ______ (HMS) _______ CHECS | CHECS HMS HARDWARE | 10.75 | 58017 | ||||||||||
48 | CHeCS-HMS | SEG46117646-307 | “_____ CTB, c_______ ______ __ ____________ _____” | “CARGO TRANSFER BAG, ACOUSTIC COUNTERMEASURE” | 1 | 5.2 | 42.6 | 24.8 | 26.7 | 5.2 | 28208 | RB | “Kit contains a sound level meter and audio dosimeters for measuring noise levels as well as ear plugs for protection. The audio dosimeters and sound level meter calibrations expired 2/06. MORD Rev B 5.7.3, GGR&C. Priority 2” | |
49 | CHeCS-HMS | SEG46117646-302 | __________ _____ ___ ________ | CARGO TRANSFER CASE ASSEMBLY HALF-SIZE | 1 | 5.3 | 42.6 | 24.8 | 26.7 | 5.3 | 28208 | RB | ACK contains headsets as well as ear plugs for hearing protection and assessment. This kit is replacing worn/broken hardware onboard. MORD | |
50 | CHeCS-HMS | SDG42104617-301 | ________ ______ __8+ | EC8+ CARTRIDGE ASSEMBLY | 25 | .01 | 9.7 | 6.6 | 1 | .25 | 1600 | HZ | “Cartridges are used with the PCBA and need to be resupplied due to their limited life (4 months). The PCBA provides information about blood constituents during PHS. These items will be stowed inside the AMP and will not impact on-orbit stowage. MORD Rev B 4.3.4.6 A, GGR&C Priority 2.” | |
51 | ____________ ___ _____ | EVA EQUIPMENT | 3.03 | 15447 | The following 23P manifest request (MR) includes EMU back-up hardware (i.e. EMU gloves) needed to support ISS-14 crewmember M. Lopez-Alegria who is launching on 13S. This MR supports the current EMU logistics plan for ISS-14 crewmember M. Lopez-Alegria. | |||||||||
52 | EVAS | 0106-110106-09 | “_____________ _________ EMU ____ VI, _ __________, 12 _” | “EMU GLOVES, 12V HEATED, PHASE VI” | 1 | 1.4 | 12.7 | 14 | 43.4 | 1.4 | 7723 | See Above | ||
53 | EVAS | 0106-110106-10 | “_____________ _________ EMU ____ VI, _ __________, 12 _” | “EMU GLOVES, 12V HEATED, PHASE VI” | 1 | 1.4 | 12.7 | 14 | 43.4 | 1.4 | 7723 | See Above | ||
54 | EVAS | SED13101715-706 | ________ _____ _________ _______ ________ __________ _________ EMU | “COVER, PROTECTIVE, LOWER ARM WRIST DISCONNECT” | 1 | .11 | .11 | See Above | ||||||
55 | EVAS | SED13101715-706 | ________ _____ _________ _______ ________ __________ _________ EMU | “COVER, PROTECTIVE, LOWER ARM WRIST DISCONNECT” | 1 | .11 | .11 | See Above | ||||||
56 | ____-__ _________-___ __________ __________ _____ _ _______-_ _________-__ ECLSS | ECLSS | 3.19 | 12504 | ||||||||||
57 | ECLSS-THC | 1F15833-1 | “______ ____________ __________ (IMV), ____________ __ ____ _________” | “IMV VALVE, LAUNCH CONFIGURATION” | 1 | 3.18 | 34 | 19.8 | 18.5 | 3.18 | 12503 | “1,Q” | “The Lab Forward Port IMV Valve must be installed prior to 10A (when Node 2 is installed) to provide required ventilation between the Lab and Node 2. To allow recovery time for potential problems experienced during installation, installation of the valve is required at least 2 flights prior to 10A. As such, the valve was originally planned for launch on 12A.1. Due to constraints for scheduling the installation during 12A.1 stage and the recent availability of launch space on flight 23P, it is desirable to launch the valve on 23P. If launch on 23P is not able to be accommodated, launch on 12A.1 should proceed.” | |
58 | ECLSS-THC | 3797604-2 | _______ | IDENTIFICATION PLATE | 1 | 0 | 5.1 | 2.5 | 0 | 0 | 0 | “1,Q” | “Installation of the nameplates ( p/n 3258303-1,p/n 3797604-2) is required per SSCM 8148 when the new IMV Valve, part number 2353024-1-1, is installed in the ISS. The IMV valve and the nameplates ( p/n 3258303-1,p/n 3797604-2) are part of a Mod Kit, Part Number 683-63417-4, defined on SSCM 8148 and must be installed together.” | |
59 | ECLSS-THC | 3258303-1 | _______ | IDENTIFICATION PLATE | 2 | 0 | 0 | 5.8 | 2.6 | .01 | 1 | “1,Q” | See Above | |
60 | ________ ___.________ | PAYLOADS | 21.08 | 121940 | ||||||||||
61 | _____-______ (COLDBAG) _ ______ ICEPAC (__ _____) | COLDBAG & ICEPACS | 21.08 | 121940 | The Coldbag hardware is being added to support future returns of cold samples on future return flights. | |||||||||
62 | PAYLOADS | SEG39136375-301 | _________ ________________ _____ ___ ________ ________ | SINGLE COLD INSULATED SAMPLE BAG | 2 | 4.5 | 22 | 25.3 | 51.3 | 9 | 57182 | HZ | See Above | |
63 | PAYLOADS | SEG39136374-301 | _______ ________________ _____ ___ ________ ________ | DOUBLE COLD INSULATED SAMPLE BAG | 1 | 8.2 | 44 | 25.3 | 51.3 | 8.2 | 57182 | HZ | The addition of cold stowage hardware to 23P is required to support the return of future payload samples on Shuttle. | |
64 | PAYLOADS | SEG33118113-315 | ________ ___________ ______ Icepac _ ____________ ___ ________ | “ICEPAC ASSY, CAPSULE STOWAGE” | 4 | .97 | 3.8 | 14 | 35.6 | 3.88 | 7576 | HZ | See Above | |
65 | _______ ___________ ___________ PCS | PCS | 4.5 | 23036 | ||||||||||
66 | CDH-PCS | 1F15351-1 | “_________ ______, ________ ____ _________ ETHERNET – ______ NODE 1 (W0939)” | “CABLE ASSY, ETHERNET, EXTERNAL – NODE 1 (W0939)” | 1 | 4.5 | 1300 | 4.7 | 4.5 | 23036 | “CR 3370 (RS C&C) provides external Ethernet cabling from the Russian Segment (RS) to the USOS. This cabling enables Command and Control of the RS avionics via a laptop in the USOS in the event that the RS has to be evacuated. The capability provided by this Ethernet connection directly enhances crew safety. There are no constraints in its use by any other project, although CR 7385 (ISL) builds upon it. All cables have been certified for Russian vehicle launch. CR 3370 installation is a precursor for ISL. Having this hardware on station (pre-positioned) will allow for it to be put in place during the first available EVA. Connectivity is an Increment 15 task.. Impact of Non-Incorporation: Increased network functionality will not be available.” | |||
67 | ________ ___.________ | PAYLOADS | 11 | 7884 | ||||||||||
68 | ______-_ _ __________-__ ___ _________ _____-__ ____-_ _ ____________ (SPHERES) | “SYNCHRONIZED POSITION, HOLD, ENGAGE, RE-ORIENT EXPERIMENTAL SATELLITES” | 11 | 7884 | The SPHERES hardware are consumables that allow SHERES experiment operation. | |||||||||
69 | PAYLOADS | SPH-1-0500-210 | ______ _ __________ _____ ___ ____________ SPHERES | SPHERES CARBON DIOXIDE TANK | 10 | .64 | 20.3 | 5.1 | 5.1 | 6.4 | 5244 | HZ | See Above | |
70 | PAYLOADS | SPH-1-0800-020 | __________ ____ _______ ___ ____________ SPHERES | SPHERES BATTERY PACK | 20 | .23 | 6.4 | 3.6 | 5.8 | 4.6 | 2640 | “BT,HZ” | See Above | |
71 | _______ ___________ ___________ PCS | PCS | 25.2 | 28401 | ||||||||||
72 | CDH-PCS | 1F15350-1 | “_________ ______, __________ ____ _________ ETHERNET – ______ NODE 1 (W0208)” | “CABLE ASSY, ETHERNET, INTERNAL – NODE 1 (W0208)” | 1 | 2.03 | 390 | 5.3 | 2.03 | 8442 | 1 | “Installation of the ISL provides new integrated Ethernet network that will provide increased bandwidth, telemetry, and COM between all partners long term.” | ||
73 | OPS LAN | 8271581-901 | ISL ROUTER ASSY | 1 | 7.33 | 31.8 | 15.2 | 20.3 | 7.34 | 9832 | “1,W” | “Installation of the ISL provides new integrated ethernet network that will provide increased bandwidth, telemetry and COM between all partners long term. Once installation is complete, the ISL will provide an Ethernet Link between the Russian Segment and the US On-Orbit Segment to allow an RS laptop in the USOS to communicate with the RS on-board computer system. In event that an emergency forces the evacuation of the RS, the crew will be able to have full insight into the RS telemetry as well as issue commands from the RS laptop in the US Segment.” | ||
74 | OPS LAN | 683-95069-1 | “_________ ____ ___ ______ _______ __ _____________ EDGE, W5069” | WIRE HARNESS ASSY – POWER TO EDGE ROUTER W5069 | 1 | 1.81 | 1036.3 | 1.3 | 1.9 | 1313 | 1 | See Above | ||
75 | OPS LAN | 683-95071-1 | “_________ ____, W5071, ______ ISL” | WIRE HARNESS ASSY – ISL CONSOLE CABLE W5071 | 1 | .95 | 609.6 | .6 | .95 | 193 | 1 | See Above | ||
76 | OPS LAN | 683-63426-3 | _______ _________ – ______ US Lab | STRUCTURAL BRKT ASSY – US LAB | 1 | .27 | 15.2 | 30.5 | 1.3 | .27 | 590 | 1 | See Above | |
77 | OPS LAN | 683-63430-1 | _________ ________ _____ Seatrac | “CABLE RESTRAINT, SEATRAC” | 3 | 1 | See Above | |||||||
78 | OPS LAN | 683-63424-1 | “_____________ ___, 2,01 _ 1,36” | “THERMAL PAD, 2.01 X 1.36” | 18 | .5 | .3 | 1 | See Above | |||||
79 | OPS LAN | 683-63424-2 | “_____________ ___, 1,88 _ 1,36” | “THERMAL PAD, 1.88 x 1.36” | 6 | 1 | See Above | |||||||
80 | OPS LAN | T30M2HALC2 | ___________ _________ | WIRE TIES | 75 | 1 | See Above | |||||||
81 | OPS LAN | REZ200 | ___________ ________ | WIRE TIE | 10 | 1 | See Above | |||||||
82 | OPS LAN | 170091 | _________ ______ | WRAP TIE | 10 | 1 | See Above | |||||||
83 | OPS LAN | 170782 | _________ ______ | WRAP TIE | 10 | 1 | See Above | |||||||
84 | OPS LAN | 170790 | _________ ______ | WRAP TIE | 10 | 1 | See Above | |||||||
85 | OPS LAN | 683-56201-11 | _________ | JUMPER ASSY | 1 | 1 | See Above | |||||||
86 | OPS LAN | 683-62416-1 | ________ ______________ ER – ______ US Lab | “ER PLATE ASSY, US LAB” | 1 | 9.53 | 63.5 | 20.3 | 5.3 | 9.53 | 6883 | 1 | See Above | |
87 | OPS LAN | 683-63426-1 | ____ ______ – ______ US Lab | STRUCTURAL CLAMP ASSY – US LAB | 1 | 1.59 | 5.1 | 8.9 | 12.7 | 1.59 | 574 | 1 | See Above | |
88 | OPS LAN | 683-63426-2 | ____ ______ – ______ US Lab | STRUCTURAL CLAMP ASSY – US LAB | 1 | 1.59 | 5.1 | 8.9 | 12.7 | 1.59 | 574 | 1 | See Above |
Notes:
BT ITEM INCLUDES BATTERIES
HZ “ITEM CONTAINS CHEMICAL, BIOLOGICAL, OR RADIOACTIVE MATERIALS OR BATTERIES”
L EARLY RETRIEVAL REQUESTED
Q LOGISTICS & MAINTENANCE (L&M) ALLOCATION – INCLUDES SYSTEM SPARES AND IVA TOOLS
R THIS HARDWARE CAN BE OPERATED IN THE RUSSIAN SEGMENT ONLY AFTER CERTIFICATION AND ACCEPTANCE IS COMPLETE.
RB CONTENTS OF THE BAG TO BE USED IN THE RUSSIAN SEGMENT
W REQUIRED ON-ORBIT POWER
FLIGHT SPECIFIC NOTES
1 Installed during Increment