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 B: SRM TEAM
ANALYSES
Figure B.20. Response of O-Ring Compressed to .046 IN.
(Linear Elastic Response, No Pressure).
Figure B19 |
Back | Figure
B21