This is an archive of information released in the past. Disclaimer: It may contain broken links or outdated information. Some parts may not function in current web browsers.
 
ISS TopJAXA Top  sitemap
 

ISS and Kibo

Kibo's Extravehicular Activity procedure development test No. 5 (OPS #5)

homeindexback

Astronaut Wakata conducting the test
Astronaut Wakata conducting the test
Astronaut Wakata conducting the test
OPS #5 view
WETS exterior
OPS #5 full view WETS exterior

Kibo's Extravehicular Activity (EVA) procedure development test No. 5 (OPS #5) was conducted in the Weightless Environment Test Building (WET) at Tsukuba Space Center (TKSC) from November 17 to 22, 2003.

The purpose of the OPS #5 is to perform the procedure development*1 and design validation*2 of Kibo, the Japanese Experiment Module, and of H-II Transfer Vehicle (HTV), which is now being developed by Japan for transporting cargo to the ISS.

*1: In procedure development, procedures are developed in advance for on-orbit assembly and maintenance of the ISS.
*2: Design validation seeks to validate whether Kibo has been designed to accommodate EVA maintenance activities.

What is OPS #5?

Kibo's elements will be launched to orbit in the years 2006 and 2007 in three Space Shuttle flights and will be assembled using the manipulator and EVA.

This test is conducted to establish more efficient Kibo assembly EVA procedures by confirming the details, such as assembly order and how the EVA astronauts move, and the time needed for these operations.

The purposes of this test are to develop the procedures related to Kibo Experiment Logistics Module Exposed Section (ELM-ES) and its onboard Exposed Facility payloads, and to establish EVA on-orbit assembly procedures after the launch of the ELM-ES. It also seeks to confirm the validity of EVA procedures for the Un-pressurized Logistic Carrier (ULC) of the H-II Transfer Vehicle (HTV).

In this test, astronauts in underwater space suits* confirm and validate assembly procedures using a full-scale mockup of Kibo and related tools located in the water pool in the Weightless Environment Test building (WET) in TKSC.

*An underwater space suit is a normal space suit remodeled for underwater use.

HTV Operation
HTV Launch HTV exterior Inside HTV HTV approaching ISS HTV Disposal (re-entry)
HTV Launch HTV exterior Inside HTV HTV approaching ISS HTV Disposal (re-entry)
HTV, which will be launched by the enhanced H-IIA Rocket, is a transfer vehicle to transport materials such as supply goods and various equipment to the ISS, and to return with spent equipment, used clothing, and other waste materials on the return trip.

Description of OPS #5

Layout of the mock-ups (Seen from above the pool.)
Layout of the mock-ups (Seen from above the pool.)

OPS #5 will be conducted to validate EVA procedures related to Kibo's ELM-ES and Un-pressurized Logistics Carrier (ULC) of the HTV. JAXA astronaut Wakata and NASA astronauts Leroy Chiao and David Wolf will participate as test subjects.

Astronauts work in the pool for three to four hours each day.


Kibo-Related tasks

The primary verification procedures are as follows.

  • Retest task after the design change
    Parts that have had a design change since the last test must be reconfirmed. The procedure will be verified by removing the Small Fine Arm (SFA), which is a part of Kibo's remote manipulator system (RMS), from the SFA Transportation Container (STC) on the Kibo ELM-ES.
  • Tasks yet to be conducted in the Weightless Environment Test
    The following procedures are planned to be conducted.
    • Removing the thermal insulation cover of Inter-orbit Communication System-Exposed Facility subsystem (ICS-EF) on ELM-ES.
    • Releasing the launch locks of ICS-EF on ELM-ES.
    • Separating the End Effector (EE) of Kibo's Remote Manipulator System from the Grapple Fixture (GF) on ELM-ES in case of an emergency.
    • Releasing the launch locks of payloads aboard the ELM-ES.
    • Contingency release of the Payload Attachment Mechanism (PAM) of the ELM-ES when a failure occurs.
    • Contingency separation of the Payload Interface Unit (PIU) if a failure occurs while attaching the ELM-ES and Exposed Facility (EF).

HTV-Related Tasks

The primary validation procedures are as follows.

  • Contingency separation of the EE of Canadarm 2 (Space Station Remote Manipulator System: SSRMS), which grapples Unpressurized Logistic Carrier's (ULC's) grapple fixture.
  • Contingency separation of HTV carrying ULC to separate the EE of SSRMS.
  • Contingency separation for the failure of latch release mechanism in removing the HTV-Exposed Pallet (EP) from ULC.
  • Contingency separation for the failure of Tie-down / Separation Mechanism (TSM) and Harness Separation Mechanism (HSM) in removing HTV-EP from ULC.
  • Contingency tie-down for the failure of lock mechanism in inserting the HTV-EP into the ULC.
Examples of HTV Exposed Pallet. Examples of HTV Exposed Pallet.
Examples of HTV Exposed Pallet.
Partial full-scale mockup of HTV used in the test. HTV-EP connected to the Exposed Facility.
Partial full-scale mockup of HTV used in the test. HTV-EP connected to the Exposed Facility.

Press Conference

The testing was opened to the press on November 19, 2003, with astronaut Wakata in the underwater space suit conducting the test and astronaut Hoshide providing an explanation.

Briefing was held for the press before the testing (from left: Mr. Matsueda, astronauts Leroy Chiao and Hoshide)
Briefing was held for the press before the testing (from left: Mr. Matsueda, astronauts Leroy Chiao and Hoshide)
Astronaut Hoshide giving explanation to the press
Astronaut Hoshide giving explanation to the press
Astronaut Wakata
Astronaut Wakata
Astronaut Wakata getting into the pool
Astronaut Wakata getting into the pool
Operations under water Operations under water Operations under water Operations under water
Operations under water
Operations under water Operations under water Operations under water
Operations under water

Last Updated : December 8, 2003

 Visibility Verification Test for the Visual Indicator of the Space Environment Data Acquisition Equipment-Attached Payload
homeindexback
JAXA Top Site Policy