Report of the PRESIDENTIAL COMMISSION
on the Space Shuttle Challenger Accident
Volume 4 Index
Hearings of the Presidential
Commission on the Space Shuttle Challenger Accident: February 6, 1986
to February 25, 1986
FEBRUARY 11, 1986 SESSION
[375] [Ref. 2/11-18]
BLOW-BY PRIMARY O-RING CONTINUES PAST 200 PSI.
[Ref. 2/11-19] RATIONALE FOR ACCEPTING
OBSERVED O-RING EROSION.
- JET IMPINGEMENT EROSION HAS BEEN SHOWN BY TEST AND ANALYSIS TO
BE WITHIN ACCEPTABLE LIMITS.
- ANALYSIS
- GAS FLOW
- HEAT TRANSFER
- STRUCTURAL
- TEST
- FULL SCALE MOTORS
- SUBSCALE MOTORS
- TEST OF O-RINGS AT 3000 PSI (3 TIMES MAXIMUM OPERATING
PRESSURE) WITH 2 TIMES OBSERVED EROSION.
- DETAILED POSTFLIGHT INSPECTION, ANALYSIS OF ANOMALIES, AND
RIGOROUS REVIEW PROCESS ASSURES UNDERSTANDING OF OBSERVATIONS.
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