Status Report

STS-112 External Tank Shuttle Observation Camera Briefing

By SpaceRef Editor
September 12, 2002
Filed under , ,

ET Shuttle Observation Camera STS-112 PAR

Background

Action assigned to JSC to evaluate potential locations for a Space Shuttle Vehicle Observation Camera

ET stand-alone camera located on the ET Cable Tray was recommended and approved

System Functional Description

– Camera system is designed to function independently of other Shuttle systems and provide real-time video of Shuttle launch through ET separation

– Activated during T-9 minute hold – Provides continuous Pre-launch and flight video (See page 4 for view)

  • SSV leaving pad
  • SRB separation
  • ET/Orb separation

Camera system function considered non-critical

  • – Camera system is a data gathering device
  • – No flight control function performed


ET Shuttle Observation Camera STS-112 PAR


ET Shuttle Observation Camera STS-112 PAR


ET Shuttle Observation Camera STS-112 PAR

Safety Analysis Report (SAR)/Critical Items List (CIL) Summary

– SAR performed to identify potential safety hazards associated with the ET Camera System

  • Considering the strong controls and verifications in place, the overall likelihood of occurrence of a catastrophic hazard remains “improbable”, and all hazard causes are ‘Controlled’
  • All identified hazards have been found to be controlled by design, specification, tests and/or inspections and all safety issues are closed
  • Shuttle Safety Review Panel (SSRP) SAR review completed 3/2000 – No Issues

– Failure Modes and Effects Analysis (FMEA) and Critical Items List (CIL) updated to identify

  • Criticality 1 failure modes and document retention rationale associated with the ET Camera System
  • – Criticality 1 ET Camera Components
  • — Antenna (4.2.14.1) (303 Stainless Steel)
  • — Camera Fairing (4.3.126.1) ( Al 2219)
  • – Criticality 1 Failure modes of the new CILs are structural failure and effects are due to debris potential to the Orbiter
  • – CIL Retention Rationale presented to the SSRP 5/2002 and PRCB 6/2002 – No Issues


ET Shuttle Observation Camera STS-112 PAR

Flight Hardware Certification Summary

Test

Camera System Hardware Qualification Testing complete – No issues

  • — System EMI Testing
  • — Fairing, Antenna and Electronics Box vibration
  • — RF and corona testing
  • — Electronics Box proof and explosive environments testing

Camera System Hardware Acceptance Testing complete – No issues

  • — Functional verification of components
  • — Electronics box vibration and thermal cycling
  • — Antenna pattern verification
  • — Camera and electronics burn-in

Camera System Functional Testing at MAF complete – No Issues

  • — Battery charge, camera function, transmitter function, dedfacing


ET Shuttle Observation Camera STS-112 PAR

Flight Hardware Certification Summary (continued)

– Analysis

— Stress Analysis on system components complete – No issues

  • — Factor of safety greater than 2.0 for all new hardware
  • — Incorporates Aerodynamic and Delta Atmospheric Pressure Loading, Random Vibration Effects, and

— Thermally Induced Stresses
— Thermal Analysis on Components Complete – No Issues

  • —Temperatures were within acceptable limits and were incorporated into stress analysis

Demonstration

  • – All work performed by certified technicians
  • — Non-standard work validated at MAF and demonstrated at KSC

Inspection

  • – System installation verified by Government Mandatory quality inspections

Certificate of Qualification approved (Reference COQ MMC-ET-TM06-127)


ET Shuttle Observation Camera STS-112 PAR

Rationale for Flight

– Camera system design fully qualified by test and analysis

  • — Acceptance testing successfully performed
  • — Functional test showed nominal performance
  • —Integrated functional tests planned after STS-112 rollout
  • — Stress Analysis ensures greater than 2.0 FS
  • — Thermal analysis ensures temperature within acceptable limits

– Camera system installation verified by demonstration and inspection

  • — Installation performed by certified technicians with validated and demonstrated processes
  • — Camera system inspection performed during and after installation

S&MA Recommendation

– STS-112/ET-115 Shuttle Observation Camera is safe to fly






SpaceRef staff editor.