Report of the PRESIDENTIAL COMMISSION
on the Space Shuttle Challenger Accident
Volume 2
Appendix H - Flight Readiness Review Treatment of
O-ring Problems
![charts 153-154 [Chart 153: Variation of Predicted SRM Erosion Depth With Heat Loss Coefficient CQ and Jet Width Wjet; Chart 154: Simulation of Nozzle Joint Primary O-ring]](https://www.nasa.gov/wp-content/uploads/static/history/rogersrep/v2h78.jpg)
Charts 153-154 [Chart 153: Variation of Predicted SRM
Erosion Depth With Heat Loss Coefficient CQ and Jet Width Wjet; Chart
154: Simulation of Nozzle Joint Primary O-ring]
Charts 151-152 |
Appendix H | Charts
155-156