Integrated cargo carrier

Last updated
Integrated cargo carrier structure Integrated Cargo Carrier.jpg
Integrated cargo carrier structure
ICC frame ICC config 2.png
ICC frame
Astronauts and technicians give a sense of scale to the ICC KSC-99PP-1425 STS-101.jpg
Astronauts and technicians give a sense of scale to the ICC

Integrated Cargo Carrier (ICC) was a project, started in 1997 by the companies Spacehab and Airbus DS Space Systems (formerly Astrium North America), [1] to develop a family of flight proven and certified cross-the-bay cargo carriers designed to fly inside the Space Shuttle 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.

Contents

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 International Space Station (ISS), transporting more than 50 unpressurized cargo elements (over 34,000 pounds) into orbit and providing for permanent attachment of two External Stowage Platforms (ESP-2 and ESP-3) to the ISS.

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 Kennedy Space Center for orbiter installation. Due to its modular design and versatility, options to adapt the ICC design to new commercial orbital space transportation vehicles exist.

Variations

Four types of ICC carriers have flown into orbit aboard the Space Shuttle:

The ICC-G is a horizontal cross-bay carrier consisting primarily of two components:

  1. A riveted, aluminum grid-type pallet structure, called the Unpressurized Cargo Pallet (UCP) and
  2. A keel yoke, called Keel Yoke Assembly (KYA).

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 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: STS-96/2A.1, STS-101/2A.2a, STS-106/2A.2b, STS-102/5A.1, STS-105/7A.1, STS-121/ULF1.1 and STS-116/12A.1.

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 grapple fixtures, 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 External Stowage Platforms, ESP-2 (launched on STS-114/LF1) and ESP-3 (launched on STS-118/13A.1). Both ICC-GDs were deployed with Extra-vehicular activity (EVA) assistance via the orbiter's and/or ISSs robotic arm (Canadarm and Canadarm2, 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 STS-114/LF1 (ESP-2) and STS-118/13A.1 (ESP-3).

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 STS-122/1E.

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 by removing the top section and converted from a non-deployable configuration to a deployable configuration by adding a grapple fixture and scuff plates. Ths ICC-VLD flew on STS-127/2JA and STS-132/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 Canadarm and subsequent handover to the Space Station's robotic arm Canadarm2. While grappled to the Space Station's robotic arm, the ICC-VLD's cargo elements, called Orbital Replacement Units ORUs were transferred with Extra-vehicular activity (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 STS-127/2JA and STS-132/ULF4.

Cargo items were installed to the UCP either via the Passive FRAM (Flight Releasable Attachment Mechanisms) 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 ISS, on board a launch vehicle or grappled by a robotic arm.

ICC Flights

FlightLaunch DatePayload/Cargo Manifest (Shuttle and ICC)
STS-96/2A.105/27/99SPACEHAB DM, ICC-G (w/ STRELA, ORU Transfer Device (both up) & SHOSS Box up/down) [2]
STS-101/2A.2a05/19/00SPACEHAB DM, ICC-G (w/ STRELA (up), SHOSS Box & SOAR both up/down) [3]
STS-106/2A.2b09/08/00SPACEHAB DM, ICC-G (w/ SOAR & SHOSS Box both up/down) [4]
STS-102/5A.103/08/01MPLM-1 ‘Leonardo’, ICC-G (w/ ESP-1, PFCS, LCA, EAS, RU all up) [5]
STS-105/7A.108/10/01MPLM-1 ‘Leonardo’, ICC-G (w/ EAS up & MISSE 1 & 2 all up) [6]
STS-114/LF107/26/05MPLM-2 ‘Raffaello’, ICC-GD/ESP-2 (w/ VSSA, MBSU, FHRC, UTA, all up as ESP-2 stayed on-orbit) [7]
STS-121/ULF1.107/04/06MPLM-1 ‘Leonardo’, ICC-G (w/ PM (up) & TUS-RA (new up/old down), and FGB) [8]
STS-116/12A.112/09/06ITS P5, Spacehab LSM, ICC-G (w/ SMDP2/3/4, SMDP Adapter up & STP-H2 launch canister up/down) [9]
STS-118/13A.108/08/07ITS S5, Spacehab LSM, ICC-GD/ESP-3 (w/ P/R-J, CMG, NTA, BCDU, ATA FSE all up as ESP-3 stayed on-orbit) [10]
STS-122/1E02/07/08COF ‘Columbus’ & ICC-L (w/ EuTEF & SOLAR (both up) & NTA up/down) [11]
STS-127/2J/A07/15/09JEM EF & ELM-ES, ICC-VLD (w/ SGANT, LDU, PM (all 3 up) & 6 P6 Batteries (new up/old down)) [12]
STS-132/ULF-405/14/10MRM-1, ICC-VLD (w/ EOTP, SGANT & Boom (up), 6 P6 Batteries (new up/old down)) [13]

See also

Related Research Articles

<i>Columbus</i> (ISS module) ESA science observatory on the International Space Station

Columbus is a science laboratory that is part of the International Space Station (ISS) and is the largest single contribution to the ISS made by the European Space Agency (ESA).

<i>Kibō</i> (ISS module) Japanese ISS module, used on ISS press conferences

The Japanese Experiment Module (JEM), nicknamed Kibō, is a Japanese science module for the International Space Station (ISS) developed by JAXA. It is the largest single ISS module, and is attached to the Harmony module. The first two pieces of the module were launched on Space Shuttle missions STS-123 and STS-124. The third and final components were launched on STS-127.

Mobile Servicing System Robotic system on board the International Space Station

The Mobile Servicing System (MSS), is a robotic system on board the International Space Station (ISS). Launched to the ISS in 2001, it plays a key role in station assembly and maintenance; it moves equipment and supplies around the station, supports astronauts working in space, and services instruments and other payloads attached to the ISS and is used for external maintenance. Astronauts receive specialized training to enable them to perform these functions with the various systems of the MSS.

STS-88 First Space Shuttle mission to the International Space Station

STS-88 was the first Space Shuttle mission to the International Space Station (ISS). It was flown by Space Shuttle Endeavour, and took the first American module, the Unity node, to the station.

STS-102 Space Shuttle mission to the International Space Station

STS-102 was a Space Shuttle mission to the International Space Station (ISS) flown by Space Shuttle Discovery and launched from Kennedy Space Center, Florida. STS-102 flew in March 2001; its primary objectives were resupplying the ISS and rotating the Expedition 1 and Expedition 2 crews. At eight hours 56 minutes, the first EVA performed on the mission remains the longest spacewalk ever undertaken.

Canadarm Robotic arm used to manoeuvre and capture mission payloads on the Space Shuttle

Canadarm or Canadarm1 is a series of robotic arms that were used on the Space Shuttle orbiters to deploy, manoeuvre, and capture payloads. After the Space Shuttle Columbia disaster, the Canadarm was always paired with the Orbiter Boom Sensor System (OBSS), which was used to inspect the exterior of the shuttle for damage to the thermal protection system.

Dextre Robotic Arm

Dextre, also known as the Special Purpose Dexterous Manipulator (SPDM), is a two armed robot, or telemanipulator, which is part of the Mobile Servicing System on the International Space Station (ISS), and does repairs otherwise requiring spacewalks. It was launched March 11, 2008 on mission STS-123.

European Robotic Arm Robotic arm installed on the ISS Russian Segment

The European Robotic Arm (ERA) is a robotic arm that is attached to the Russian Orbital Segment (ROS) of the International Space Station. Launched to the ISS in 2021; it is the first robotic arm that is able to work on the Russian Segment of the station. The arm supplements the two Russian Strela cargo cranes that were originally installed on the Pirs module, but were later moved to the docking compartment Poisk and Zarya module.

Astrotech Corporation, formerly Spacehab Inc., is a technology incubator headquartered in Austin, Texas. Astrotech uses technology sourced internally and from research institutions, government laboratories, and universities to fund, manage and sell start-up companies.

External stowage platform

External stowage platforms (ESPs) are key components of the International Space Station (ISS). Each platform is made from steel and serves as an external pallet that can hold spare parts, also known as orbital replacement units (ORUs), for the space station. As a platform it is not pressurized, but does require electricity to power the heaters of some of the stored equipment. ORUs are attached to the ESP via Flight Releasable Attachment Mechanisms (FRAMs), matching witness plates that mate the ORU to the platform.

STS-127 Space Shuttle mission to the International Space Station

STS-127 was a NASA Space Shuttle mission to the International Space Station (ISS). It was the twenty-third flight of Space ShuttleEndeavour. The primary purpose of the STS-127 mission was to deliver and install the final two components of the Japanese Experiment Module: the Exposed Facility, and the Exposed Section of the Experiment Logistics Module (ELM-ES). When Endeavour docked with the ISS on this mission in July 2009, it set a record for the most humans in space at the same time in the same vehicle, the first time thirteen people have been at the station at the same time. Together they represented all ISS program partners and tied the general record of thirteen people in space with the first such occurrence of 1995.

STS-132 2010 Space Shuttle "Atlantis" mission to dock with the ISS

STS-132 was a NASA Space Shuttle mission, during which Space Shuttle Atlantis docked with the International Space Station on 16 May 2010. STS-132 was launched from the Kennedy Space Center on 14 May 2010. The primary payload was the Russian Rassvet Mini-Research Module, along with an Integrated Cargo Carrier-Vertical Light Deployable (ICC-VLD). Atlantis landed at the Kennedy Space Center on 26 May 2010.

ExPRESS Logistics Carrier Module on the International Space Station

An EXpedite the PRocessing of Experiments to Space Station (ExPRESS) Logistics Carrier (ELC) is an unpressurized attached payload platform for the International Space Station (ISS) that provides mechanical mounting surfaces, electrical power, and command and data handling services for Orbital Replacement Units (ORUs) as well as science experiments on the ISS. The ELCs were developed primarily at the Goddard Space Flight Center in Greenbelt, Maryland, with support from JSC, KSC, and MSFC. ELC was formerly called "Express Pallet" and is the unpressurized counterpart to the pressurized ExPRESS Rack. An ELC provides scientists with a platform and infrastructure to deploy experiments in the vacuum of space without requiring a separate dedicated Earth-orbiting satellite.

Grapple fixture

Grapple fixtures are used on spacecraft or other objects to provide a secure connection for a robotic arm.

STS-134 25th and last spaceflight of Space Shuttle Endeavour

STS-134 was the penultimate mission of NASA's Space Shuttle program and the 25th and last spaceflight of Space ShuttleEndeavour. This flight delivered the Alpha Magnetic Spectrometer and an ExPRESS Logistics Carrier to the International Space Station. Mark Kelly served as the mission commander. STS-134 was expected to be the final space shuttle mission if STS-135 did not receive funding from Congress. However, in February 2011, NASA stated that STS-135 would fly "regardless" of the funding situation. STS-135, flown by Atlantis, took advantage of the processing for STS-335, the Launch on Need mission that would have been necessary if the STS-134 crew became stranded in orbit.

STS-135 135th and final mission of the American Space Shuttle program

STS-135 was the 135th and final mission of the American Space Shuttle program. It used the orbiter Atlantis and hardware originally processed for the STS-335 contingency mission, which was not flown. STS-135 launched on 8 July 2011, and landed on 21 July 2011, following a one-day mission extension. The four-person crew was the smallest of any shuttle mission since STS-6 in April 1983. The mission's primary cargo was the Multi-Purpose Logistics Module (MPLM) Raffaello and a Lightweight Multi-Purpose Carrier (LMC), which were delivered to the International Space Station (ISS). The flight of Raffaello marked the only time that Atlantis carried an MPLM.

Kounotori 2 Second H-II Transfer Vehicle

Kounotori 2, also known as HTV-2, was launched in January 2011 and was the second Japanese H-II Transfer Vehicle to resupply the International Space Station (ISS). It was launched by the H-IIB Launch Vehicle No. 2 manufactured by Mitsubishi Heavy Industries (MHI) and JAXA. After the supplies were unloaded, Kounotori 2 was loaded with waste material from ISS, including used experiment equipment and used clothes. Kounotori 2 was then unberthed and separated from the ISS and burned up upon reentering the atmosphere on 30 March 2011.

US Orbital Segment US components of the International Space Station

The US Orbital Segment (USOS) is the name given to the components of the International Space Station (ISS) constructed and operated by the United States National Aeronautics and Space Administration (NASA), European Space Agency (ESA), Canadian Space Agency (CSA) and Japan Aerospace Exploration Agency (JAXA). The segment currently consists of eleven pressurized components and various external elements, all of which were delivered by the Space Shuttle.

Orbital replacement unit

Orbital replacement units (ORUs) are key elements of the International Space Station that can be readily replaced when the unit either passes its design life or fails. ORUs are parts of the main systems and subsystems of the external elements of the ISS, none are intended to be installed inside the pressurised modules. Examples of ORUs are: pumps, storage tanks, controller boxes, antennas, and battery units. Such units are replaced either by astronauts during EVA or by the Dextre (SPDM) robotic arm. All are stored on the three external stowage platforms (ESPs) or the four ExPRESS Logistics Carriers (ELCs) mounted on the Integrated Truss Structure (ITS).

The Research Double Module was a payload module built by Spacehab Inc for the US Space Shuttle Orbiters.

References

  1. airbusdshouston.com
  2. "NASA Space Shuttle STS-96 Press Kit". Scribd.com. 1999-05-20. Retrieved 2013-03-27.
  3. "NASA Space Shuttle STS-101 Press Kit". Scribd.com. 2000-04-07. Retrieved 2013-03-27.
  4. "NASA Space Shuttle STS-106 Press Kit". Scribd.com. 2000-08-29. Retrieved 2013-03-27.
  5. "NASA Space Shuttle STS-102 Press Kit". Scribd.com. 2001-03-06. Retrieved 2013-03-27.
  6. "NASA Space Shuttle STS-105 Press Kit". Scribd.com. 2001-07-24. Retrieved 2013-03-27.
  7. "NASA Space Shuttle STS-114 Press Kit". Scribd.com. Retrieved 2013-03-27.
  8. "NASA Space Shuttle STS-121 Press Kit". Scribd.com. 2012-09-22. Retrieved 2013-03-27.
  9. "NASA Space Shuttle STS-116 Press Kit". Scribd.com. 2012-09-22. Retrieved 2013-03-27.
  10. "NASA Space Shuttle STS-118 Press Kit". Scribd.com. Retrieved 2013-03-27.
  11. "NASA Space Shuttle STS-122 Press Kit". Scribd.com. Retrieved 2013-03-27.
  12. "NASA Space Shuttle STS-127 Press Kit". Scribd.com. 2011-10-20. Retrieved 2013-03-27.
  13. "NASA Space Shuttle STS-132 Press Kit". Scribd.com. 2011-07-31. Retrieved 2013-03-27.