Report of the PRESIDENTIAL COMMISSION on the Space Shuttle Challenger Accident

Volume 2

Appendix L - NASA Accident Analysis Team Report. [Part 2]

STS 51-L DATA & DESIGN ANALYSIS TASK FORCE ACCIDENT ANALYSIS TEAM SOLID ROCKET MOTOR WORKING GROUP

Appendix C: SRM TEAM TESTS

Figure C.5. Batch 268635 O-ring Average Recovery During First Second After Load Release (1 Std. Dev. Scatter) Test Temperature = 25°F Initial Compression = 40 mils 2 Hour Duration.

Figure C.5. Batch 268635 O-ring Average Recovery During First Second After Load Release (1 Std. Dev. Scatter) Test Temperature = 25°F Initial Compression = 40 mils 2 Hour Duration.

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