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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:
148:, 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
226:(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
241:) 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
201:
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
107:
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
172:, 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
75:
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
188:
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
202:
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
64:
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
61:
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.
57:
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
144:
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
80:
for orbiter installation. Due to its modular design and versatility, options to adapt the ICC design to new commercial orbital space transportation vehicles exist.
892:
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210:/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
68:(ISS), transporting more than 50 unpressurized cargo elements (over 34,000 pounds) into orbit and providing for permanent attachment of two
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218:. 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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8:
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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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58:
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Four types of ICC carriers have flown into orbit aboard the Space
Shuttle:
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35:
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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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164:(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)
245:, on board a launch vehicle or grappled by a robotic arm.
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53:) was a project, started in 1997 by the companies
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42:and technicians give a sense of scale to the ICC
893:Components of the International Space Station
103:A keel yoke, called Keel Yoke Assembly (KYA).
262:Payload/Cargo Manifest (Shuttle and ICC)
160:/13A.1). Both ICC-GDs were deployed with
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26:
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239:Flight Releasable Attachment Mechanisms
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839:"NASA Space Shuttle STS-132 Press Kit"
818:"NASA Space Shuttle STS-127 Press Kit"
797:"NASA Space Shuttle STS-122 Press Kit"
776:"NASA Space Shuttle STS-118 Press Kit"
755:"NASA Space Shuttle STS-116 Press Kit"
734:"NASA Space Shuttle STS-121 Press Kit"
713:"NASA Space Shuttle STS-114 Press Kit"
692:"NASA Space Shuttle STS-105 Press Kit"
671:"NASA Space Shuttle STS-102 Press Kit"
650:"NASA Space Shuttle STS-106 Press Kit"
629:"NASA Space Shuttle STS-101 Press Kit"
608:"NASA Space Shuttle STS-96 Press Kit"
197:ICC-VLD (Vertical Light Deployable)
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23:Integrated cargo carrier structure
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863:Airbus DS Space Systems, Inc.
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156:/LF1) and ESP-3 (launched on
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572:International Space Station
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140:ICC-GD (Generic Deployable)
66:International Space Station
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150:External Stowage Platforms
70:External Stowage Platforms
567:External Stowage Platform
841:. Scribd.com. 2011-07-31
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652:. Scribd.com. 2000-08-29
631:. Scribd.com. 2000-04-07
610:. Scribd.com. 1999-05-20
224:Extra-vehicular activity
162:Extra-vehicular activity
47:Integrated Cargo Carrier
222:were transferred with
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152:, ESP-2 (launched on
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873:NASA videos of ESP-2
78:Kennedy Space Center
16:Space Shuttle module
878:shuttlepresskit.com
596:airbusdshouston.com
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176:/LF1 (ESP-2) and
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180:/13A.1 (ESP-3).
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92:ICC-G (Generic)
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184:ICC-L (Light)
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132:/ULF1.1 and
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519:ICC STS-116
507:ICC STS-121
493:ICC STS-105
481:ICC STS-102
469:ICC STS-106
457:ICC STS-101
259:Launch Date
249:ICC Flights
845:2013-03-27
824:2013-03-27
803:2013-03-27
782:2013-03-27
761:2013-03-27
740:2013-03-27
719:2013-03-27
698:2013-03-27
677:2013-03-27
656:2013-03-27
635:2013-03-27
614:2013-03-27
583:References
445:ICC STS-96
84:Variations
40:Astronauts
230:/2JA and
216:Canadarm2
206:/2JA and
170:Canadarm2
31:ICC frame
887:Category
561:See also
427:05/14/10
413:07/15/09
399:02/07/08
385:08/08/07
371:12/09/06
357:07/04/06
343:07/26/05
329:08/10/01
315:03/08/01
301:09/08/00
287:05/19/00
273:05/27/99
212:Canadarm
166:Canadarm
136:/12A.1.
120:/2A.2b,
116:/2A.2a,
55:Spacehab
422:STS-132
408:STS-127
394:STS-122
380:STS-118
366:STS-116
354:/ULF1.1
352:STS-121
338:STS-114
324:STS-105
310:STS-102
296:STS-106
282:STS-101
234:/ULF4.
232:STS-132
228:STS-127
208:STS-132
204:STS-127
191:STS-122
178:STS-118
174:STS-114
158:STS-118
154:STS-114
134:STS-116
130:STS-121
128:/7A.1,
126:STS-105
124:/5A.1,
122:STS-102
118:STS-106
114:STS-101
112:/2A.1,
424:/ULF-4
382:/13A.1
368:/12A.1
298:/2A.2b
284:/2A.2a
268:STS-96
256:Flight
110:STS-96
410:/2J/A
326:/7A.1
312:/5A.1
270:/2A.1
193:/1E.
340:/LF1
220:ORUs
168:and
396:/1E
243:ISS
51:ICC
889::
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49:(
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