An Heritage Approach to Aerospace Risk Based Design: With ...
An Heritage Approach to Aerospace Risk Based Design: With ...
An Heritage Approach to Aerospace Risk Based Design: With ...
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Potential Impact of Candidate<br />
Technologies<br />
Continued component reliability improvements become less important<br />
<strong>Risk</strong> Contribu<strong>to</strong>rs for Shuttle Baseline with<br />
improving SSME<br />
LOV Probability (per<br />
mission)<br />
28-29 Oc<strong>to</strong>ber 2002<br />
Slide 23 of 42<br />
6.00E-03<br />
5.00E-03<br />
4.00E-03<br />
3.00E-03<br />
2.00E-03<br />
1.00E-03<br />
0.00E+00<br />
1.00E-08<br />
4.9.E-08<br />
1.0.E-07<br />
3.0.E-07<br />
5.0.E-07<br />
8.0.E-07<br />
1.0.E-06<br />
1.3.E-06<br />
Engine Failure Rate (eng-sec)<br />
A <strong>Heritage</strong> <strong>Approach</strong> <strong>to</strong> <strong>Aerospace</strong> <strong>Risk</strong> <strong>Based</strong> <strong>Design</strong>: <strong>With</strong> Application<br />
Day 1 Afternoon<br />
LOV-LD<br />
LOV-FC<br />
LOV-TPS<br />
LOV-ET-ASC<br />
LOV-BOOST-ASC<br />
LOV-ORB-ASC
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