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of the UCP. The KYA is a U-shaped structure whose primary purpose is to transfer UCP loads to the
Orbiter via longeron and keel trunnions. The KYA’s design allowed it to be installed under pressurized tunnel sections in the Orbiter payload bay, thereby allowing the ICC-G to be used in conjunction with a SPACEHAB pressurized module. The ICC-G flew on seven Space Shuttle missions:
159:, scuff plates and a deployment kit to allow UCP separation from the KYA. The UCP is deployed while the KYA remains in the Orbiter cargo bay. On-orbit, the UCP can be removed from the Orbiter payload bay, used as a payload / experiment platform, and returned to the payload bay on the same or a subsequent flight. Two ICC-GDs were launched and permanently attached to the ISS as
237:(EVA) assistance to the respective locations on the ISS. The ICC-VLD provided heater power and electrical connections for the ORUs while inside the cargo bay or grappled by the robotic arm. Upon completion of ORU removal and replacement activities (R&R), the ICC-VLDs were both berthed back into the orbiter and returned to earth. The ICC-VLD flew on the Shuttle missions
252:) Adapter Plate (PFRAM) (for ORUs) or mounted directly to the UCP's node hole or peripheral hole pattern. The general ICC design also incorporates avionic systems allowing for on-board data acquisition/processing/WLAN via integrated computer as well as power distribution for the cargoes via Power Distribution Unit (PDU) while installed on the
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The ICC-VLD is a derivative of the not-flown ICC-V. Due to the modular pallet design of the ICC-V which is composed of one central core section and two identical outer sections that bolt to the upper and lower edges of the core section, the ICC-VLD is converted from the octagonal-shaped ICC-V design
118:
The UCP is the primary structural element of the ICC that provides structural support for payload items carried in the unpressurized volume of the
Orbiter’s cargo bay. The ICC-G UCP's dimensions are approx. 14 feet (width) × 8.5 feet (length) × 10 inches (thick). Cargoes can be mounted on both faces
183:, respectively). The ESP-2 and ESP-3 provides electrical power to the ORUs while attached to the ISS via the ICC-GDs Power Distribution Unit (PDU) and power cable/PCAS (Passive Common Attach System) interface. The ICC-GD flew on the Shuttle missions
86:
Airbus' former Cape
Canaveral integration facility, which was located at Astrotech's processing facility (formerly SPACEHAB Payload Processing Facility (SPPF)) provided for the physical integration of cargoes to the ICC and subsequent transport to
199:
The ICC-L is the principal one half of an ICC-G, using the removable core section from the not-flown ICC-V (Vertical) rotated into a horizontal orientation and combining it with the KYA. The ICC-L flew once on
213:
by removing the top section and converted from a non-deployable configuration to a deployable configuration by adding a grapple fixture and scuff plates. The ICC-VLD flew on
75:
The ICC carriers flew on 12 Space
Shuttle missions between 1999 and 2010 under NASA's Cargo Mission Contract contributing to the construction, supply and maintenance of the
72:
cargo bay, installed either horizontally or vertically, and able to carry up to 8000 lbs. of unpressurized cargo into orbit. Airbus owns the ICC fleet of carriers.
68:
and Airbus DS Space
Systems (formerly Astrium North America), to develop a family of flight proven and certified cross-the-bay cargo carriers designed to fly inside the
155:
The ICC-GD is the deployable version of the ICC-G. It consists of a UCP and a KYA (same dimensions as for ICC-G), both outfitted with deployment hardware including
91:
for orbiter installation. Due to its modular design and versatility, options to adapt the ICC design to new commercial orbital space transportation vehicles exist.
903:
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221:/ULF4. During both missions, the ICC-VLD was deployed from the orbiter's cargo bay and transferred to the ISS via the orbiter's robotic arm
79:(ISS), transporting more than 50 unpressurized cargo elements (over 34,000 pounds) into orbit and providing for permanent attachment of two
17:
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229:. While grappled to the Space Station's robotic arm, the ICC-VLD's cargo elements, called Orbital Replacement Units
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ITS S5, Spacehab LSM, ICC-GD/ESP-3 (w/ P/R-J, CMG, NTA, BCDU, ATA FSE all up as ESP-3 stayed on-orbit)
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JEM EF & ELM-ES, ICC-VLD (w/ SGANT, LDU, PM (all 3 up) & 6 P6 Batteries (new up/old down))
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ITS P5, Spacehab LSM, ICC-G (w/ SMDP2/3/4, SMDP Adapter up & STP-H2 launch canister up/down)
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A riveted, aluminum grid-type pallet structure, called the
Unpressurized Cargo Pallet (UCP) and
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MPLM-2 ‘Raffaello’, ICC-GD/ESP-2 (w/ VSSA, MBSU, FHRC, UTA, all up as ESP-2 stayed on-orbit)
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SPACEHAB DM, ICC-G (w/ STRELA, ORU Transfer Device (both up) & SHOSS Box up/down)
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The ICC-G is a horizontal cross-bay carrier consisting primarily of two components:
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MRM-1, ICC-VLD (w/ EOTP, SGANT & Boom (up), 6 P6 Batteries (new up/old down))
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COF ‘Columbus’ & ICC-L (w/ EuTEF & SOLAR (both up) & NTA up/down)
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MPLM-1 ‘Leonardo’, ICC-G (w/ PM (up) & TUS-RA (new up/old down), and FGB)
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Four types of ICC carriers have flown into orbit aboard the Space
Shuttle:
30:
46:
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SPACEHAB DM, ICC-G (w/ STRELA (up), SHOSS Box & SOAR both up/down)
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Cargo items were installed to the UCP either via the
Passive FRAM (
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MPLM-1 ‘Leonardo’, ICC-G (w/ EAS up & MISSE 1 & 2 all up)
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MPLM-1 ‘Leonardo’, ICC-G (w/ ESP-1, PFCS, LCA, EAS, RU all up)
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175:(EVA) assistance via the orbiter's and/or ISSs robotic arm (
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and subsequent handover to the Space
Station's robotic arm
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SPACEHAB DM, ICC-G (w/ SOAR & SHOSS Box both up/down)
256:, on board a launch vehicle or grappled by a robotic arm.
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64:) was a project, started in 1997 by the companies
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53:and technicians give a sense of scale to the ICC
904:Components of the International Space Station
114:A keel yoke, called Keel Yoke Assembly (KYA).
273:Payload/Cargo Manifest (Shuttle and ICC)
171:/13A.1). Both ICC-GDs were deployed with
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250:Flight Releasable Attachment Mechanisms
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850:"NASA Space Shuttle STS-132 Press Kit"
829:"NASA Space Shuttle STS-127 Press Kit"
808:"NASA Space Shuttle STS-122 Press Kit"
787:"NASA Space Shuttle STS-118 Press Kit"
766:"NASA Space Shuttle STS-116 Press Kit"
745:"NASA Space Shuttle STS-121 Press Kit"
724:"NASA Space Shuttle STS-114 Press Kit"
703:"NASA Space Shuttle STS-105 Press Kit"
682:"NASA Space Shuttle STS-102 Press Kit"
661:"NASA Space Shuttle STS-106 Press Kit"
640:"NASA Space Shuttle STS-101 Press Kit"
619:"NASA Space Shuttle STS-96 Press Kit"
208:ICC-VLD (Vertical Light Deployable)
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34:Integrated cargo carrier structure
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874:Airbus DS Space Systems, Inc.
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167:/LF1) and ESP-3 (launched on
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583:International Space Station
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151:ICC-GD (Generic Deployable)
77:International Space Station
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161:External Stowage Platforms
81:External Stowage Platforms
578:External Stowage Platform
852:. Scribd.com. 2011-07-31
831:. Scribd.com. 2011-10-20
768:. Scribd.com. 2012-09-22
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705:. Scribd.com. 2001-07-24
684:. Scribd.com. 2001-03-06
663:. Scribd.com. 2000-08-29
642:. Scribd.com. 2000-04-07
621:. Scribd.com. 1999-05-20
235:Extra-vehicular activity
173:Extra-vehicular activity
58:Integrated Cargo Carrier
18:Integrated Cargo Carrier
233:were transferred with
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163:, ESP-2 (launched on
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884:NASA videos of ESP-2
89:Kennedy Space Center
27:Space Shuttle module
889:shuttlepresskit.com
607:airbusdshouston.com
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187:/LF1 (ESP-2) and
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191:/13A.1 (ESP-3).
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854:. Retrieved
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143:/ULF1.1 and
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530:ICC STS-116
518:ICC STS-121
504:ICC STS-105
492:ICC STS-102
480:ICC STS-106
468:ICC STS-101
270:Launch Date
260:ICC Flights
856:2013-03-27
835:2013-03-27
814:2013-03-27
793:2013-03-27
772:2013-03-27
751:2013-03-27
730:2013-03-27
709:2013-03-27
688:2013-03-27
667:2013-03-27
646:2013-03-27
625:2013-03-27
594:References
456:ICC STS-96
95:Variations
51:Astronauts
241:/2JA and
227:Canadarm2
217:/2JA and
181:Canadarm2
42:ICC frame
898:Category
572:See also
438:05/14/10
424:07/15/09
410:02/07/08
396:08/08/07
382:12/09/06
368:07/04/06
354:07/26/05
340:08/10/01
326:03/08/01
312:09/08/00
298:05/19/00
284:05/27/99
223:Canadarm
177:Canadarm
147:/12A.1.
131:/2A.2b,
127:/2A.2a,
66:Spacehab
433:STS-132
419:STS-127
405:STS-122
391:STS-118
377:STS-116
365:/ULF1.1
363:STS-121
349:STS-114
335:STS-105
321:STS-102
307:STS-106
293:STS-101
245:/ULF4.
243:STS-132
239:STS-127
219:STS-132
215:STS-127
202:STS-122
189:STS-118
185:STS-114
169:STS-118
165:STS-114
145:STS-116
141:STS-121
139:/7A.1,
137:STS-105
135:/5A.1,
133:STS-102
129:STS-106
125:STS-101
123:/2A.1,
435:/ULF-4
393:/13A.1
379:/12A.1
309:/2A.2b
295:/2A.2a
279:STS-96
267:Flight
121:STS-96
421:/2J/A
337:/7A.1
323:/5A.1
281:/2A.1
204:/1E.
351:/LF1
231:ORUs
179:and
407:/1E
254:ISS
62:ICC
900::
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