Match the metric with it’s strategy
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Which part of the RAM RMA plan would you most likely see the…
Which part of the RAM RMA plan would you most likely see the use of digital twins?
If the LSA-R later updates the failure rate to 0.006 failure…
If the LSA-R later updates the failure rate to 0.006 failures per hour from new field data, re-compute the previous part – n=2 staged spares, compute the probability of no stockout during the mission – Solution is a percentage, round to 2 decimals (ie, 45.67)
Now, let’s apply stats/PDF/CDF to LSA & LSA-R logistics LRU…
Now, let’s apply stats/PDF/CDF to LSA & LSA-R logistics LRU = Line Replaceable Unit An LRU required for a 100-hour mission has a constant failure rate of 0.01 failures per hour (so MTBF = 100 hours). Per the LSA-R, (for simplicity) maintenance swaps are immediate and do not consume mission time. You position/stage (keep) n spares of this LRU at the point of use before the mission starts (so replacements are immediately available) Let N be the number of LRU failures during the mission. What distribution models N?
Let’s switch gears to PBL
Let’s switch gears to PBL
Matching: INCOSE concepts to PBL elements
Matching: INCOSE concepts to PBL elements
The continuous random variable T is used to model the number…
The continuous random variable T is used to model the number of days, t, a mosquito survives after hatching. The probability that a mosquito survives for more than t days is:
To ensure that an approved Engineering Change Order propagat…
To ensure that an approved Engineering Change Order propagates automatically into updated crew maintenance procedures without manual re-entry, which artifact must be the configuration-controlled ASOT across contractors?
Hypothetical situation: During Test & Evaluation, a deficien…
Hypothetical situation: During Test & Evaluation, a deficiency is discovered. How should that flow work to minimize error?
Risk Sensitivity Index – A team runs a Monte Carlo simulatio…
Risk Sensitivity Index – A team runs a Monte Carlo simulation on failure risk for a missile guidance subsystem. The model outputs an estimated risk of failure of 0.0023 with a 95% confidence interval of ±0.0008. What are the lower and upper bounds of the 95% confidence interval? Is this system within a safety requirement that sets the max allowable failure rate at 0.003? [lower] format – 4 decimals ie, 0.1234 [upper] format – 4 decimals ie, 0.1234 [yes_no]