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Public Lessons Learned Entry: 1101

Lesson Info:

  • Lesson Number: 1101
  • Lesson Date: 2001-01-01
  • Submitting Organization: JSC
  • Submitted by: Jeff Dutton / Ronald Montague

Subject:

Hardware losses during STS-88 Extravehicular Activities (EVAs, also known as space walks)

Description of Driving Event:

Several items of EVA hardware were lost during the EVAs on STS-88. Impact to immediate mission is loss of availability of needed tools. Lost tooling, when unretrieved, also adds to on orbit debris.

  • The flight support equipment (FSE) for the EVA installable slidewire and an on-orbit installed worksite interface (OIWIF) with an attached retractable tether were lost on EVA1.
  • One of the trunnion pin covers was lost on EVA2.
  • Two of the safety tether hook guards were also lost during the EVAs.

There is no identified common hardware cause for the lost hardware. The EVA Project Office chartered a team to investigate the issue and make recommendations for corrective action.

Root cause:

  • Slidewire Carrier - inconclusive, most probable cause is inadvertent opening of Tool Stanchion bayonet.
  • On orbit installed WIF/retractable tether - inconclusive, most probable cause was the hardware was tethered to another end item and was released when that end item was removed from the mini workstation.
  • Trunnion pin cover - was not properly tethered due to a lack of a tether loop on the mockup/trainer.
  • Tether hook clips - inadequate restraint in design.

Lesson(s) Learned:

Careful planning from design through training, flight rules, and operations is required to prevent loss of equipment and tooling during space walk operations.

Recommendation(s):

Slidewire carrier - implement an operational constraint to require that items in Tool stanchion and other similar bayonets also be tethered. OIWIF/retractable tether - reemphasize crew training to visually verify hook mate/demate on mini workstation. Trunnion pin cover - update trainer to include tether loop. Tether hook clips - Include integral ring/spring to allow clip to be attached back to itself.

Evidence of Recurrence Control Effectiveness:

All the recommendations were implemented for 2A.1 with no recurrence of loss.

Documents Related to Lesson:

N/A

Mission Directorate(s):

  • Exploration Systems
  • Space Operations
  • Aeronautics Research

Additional Key Phrase(s):

  • Extra-Vehicular Activity
  • Flight Equipment
  • Hardware
  • Human Factors
  • Policy & Planning
  • Risk Management/Assessment
  • Safety & Mission Assurance
  • Spacecraft
  • Training Equipment

Additional Info:

    Approval Info:

    • Approval Date: 2002-02-12
    • Approval Name: Ronald Montague
    • Approval Organization: JSC
    • Approval Phone Number: (281) 483-8576


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