Jump to content

External stowage platform

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by Jarrod Baniqued (talk | contribs) at 04:01, 24 October 2009 (→ESP-3). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

ESP-1 can be seen as the highlighted rectangular shaped object attached to the Destiny Laboratory.

The External Stowage Platforms (ESP) are three components of the International Space Station (ISS). Each ESP is an external pallet that can hold spare parts, also known as Orbital Replacement Units (ORU), 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. The ORUs are attached to the ESP with Flight Releasable Attachment Mechanisms (FRAM). The structure of the platforms is based on the Integrated Cargo Carrier (ICC) originally designed for the Space Shuttle and produced by Spacehab, Inc.[1]

ESP-1

The first of the External Stowage Platforms, called ESP-1, was installed on the hull of the Destiny Laboratory Module on March 13, 2001 during the second EVA of the STS-102 Space Shuttle mission.[2] It is powered by the Unity Module and has two FRAMs to store ORUs.

ESP-1 holds the following ORUs:[3]

  1. Direct Current Switching Unit (DCSU)
  2. Pump Flow Control System (PFCS)

ESP-2

ESP-2 can be seen highlighted and under the Quest Joint Airlock.

ESP-2 was installed with the assistance of Space Shuttle Discovery's robotic arm and two spacewalkers during the STS-114 mission.[4] It is much larger than ESP-1 with eight FRAMs creating room for up to eight spare parts (ORUs). Like ESP-1, it is powered by the Unity Module. However unlike ESP-1, the ESP-2 is attached to the Quest Joint Airlock using a specialized ESP Attachment Device (ESPAD). As of February 2009, the ORUs on ESP-2 are:

  1. Flex Hose Rotary Coupler
  2. Main Bus Switching Unit
  3. Utility Transfer Assembly
  4. Battery Charge/Discharge Unit (BCDU)
  5. Pump Module Assembly (PMA)
  6. SPACEHAB/Oceaneering Space Systems - Extended Deployable
  7. Main Bus Switching Unit (added on October 23, 2007 during STS-120)
  8. Direct Current Switching Unit (DCSU) (added on March 17, 2008 during STS-123)
  9. Direct Current Switching Unit (DCSU) (added on March 17, 2008 during STS-123)
  10. Yaw Joint for Canadarm2 (added on March 17, 2008 during STS-123)

The four Video Stanchion Assemblies initially stored on ESP-2 were installed on the P1 truss segment on November 7, 2005, on the S1 truss segment on August 3, 2006, on the S3 truss segment during EVA 4 of STS-117 on June 17, 2007, and on the P1 truss segment during an EVA on July 23, 2007. The empty FSE/FRAM (Flight Support Equipment/Flight Releasable Attach Mechanism) was then removed from ESP-2 and jettisoned overboard on July 23, 2007. The empty VSSA FSE/FRAM was 96 kg in mass and 1.4 x 1.2 x 0.9m in size.

A failed Control Moment Gyroscope was stored on ESP-2 from August 13, 2007 (when it was removed from service during an EVA) until February 13, 2008 (when it was returned to Earth on STS-122).

ESP-3

ESP-3 being installed by Canadarm2.

ESP-3 was installed on August 14, 2007 during the Space Shuttle STS-118 mission.[5] It has eight attachment sites capable of holding up to seven ISS spare parts and assemblies. The platform also has handrails and attachment points for tethers and foot restraints that astronauts can use while working with the ORUs on the ESP-3.

ESP-3 was the first major station element to be installed completely by robotics, using only the shuttle and station’s robotic arms, an External Berthing Camera System (BCS) and a Photovoltaic Radiator Grapple Fixture (PVRGF). Astronauts robotically installed the platform onto the station's P3 truss segment during the STS-118 mission’s seventh day.[6]

As of July 2009, the following ORUs are installed on ESP-3:

  1. Battery Charge/Discharge Unit (BCDU) - A BCDU charges batteries and provides conditioned battery power to power buses during eclipse periods.
  2. Pitch Roll Joint (P/R‐J) – The P/R-J is an ORU provided by the Canadian Space Agency for the Canadarm2, the Space Station Remote Manipulator System (SSRMS).
  3. Flex Hose Rotary Coupler. Added on November 18, 2008 during STS-126.
  4. Space-to-Ground Antenna (SGANT) - a replacement Ku-band communications antenna. Added on July 20, 2009 during STS-127.
  5. Coolant system pump module (1,300 pounds). Added on July 20, 2009 during STS-127.
  6. Mobile Base Station transporter drive motor. Added on July 20, 2009 during STS-127.

The Control Moment Gyroscope (CMG) and its associated support frame that were on ESP-3 at launch were removed on August 13, 2007. The support frame was placed on ESP-2 and the CMG was installed in the Z1 truss.

The Nitrogen Tank Assembly (NTA) that was on ESP-3 at launch was moved to the S1 truss on June 8, 2008 to replace a depleted tank.

A depleted Nitrogen Tank Assembly (NTA) was stored on ESP-3 from June 8, 2008 (when it was removed from service on the S1 truss during an STS-124 EVA) until November 18, 2008 (when it was returned to Earth on STS-126).

Notes

  1. ^ Boeing ESP-2 information
  2. ^ STS-102, Mission Control Center Status Report # 11 Tuesday, March 13, 2001 7:30 a.m. CST
  3. ^ "Minutes for May 29, 2001 EVA AIT" (Press release). NASA. May 29, 2001. Retrieved 2007-08-01.
  4. ^ NASA ISS Assembly
  5. ^ NASA's consolidated Launch Manifest for ISS Assembly
  6. ^ NASA's ISS assembly information
Retrieved from "https://en.wikipedia.org/w/index.php?title=External_stowage_platform&oldid=321697743"