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A cost-benefit analysis of the doppler radar wind profiler (drwp) at the kennedy space center (ksc), using mathematical concepts such as sample space, event, probability, and mathematical expectation. The analysis aims to determine the justification for the $250,000 annual operating cost of the drwp, which is used for approximately 10 shuttle launches and 2 titan rocket launches per year.
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Project Grant Team
John S. Pazdar Patricia L. Hirschy Project Director Principal Investigator Capital Comm-Tech College Asnuntuck Comm-Tech College Hartford, Connecticut Enfield, Connecticut
This project was supported, in part, by the Peter A. Wursthorn National Science Foundation Principal Investigator Opinions expressed are those of the authors Capital Comm-Tech College and not necessarily those of the Foundation Hartford, Connecticut
NASA - AMATYC - NSF
Spinoffs are relatively short learning modules inspired by the LTAs. They can be easily
implemented to support student learning in courses ranging from prealgebra through calculus.
The Spinoffs typically give students an opportunity to use mathematics in a real world context.
Dennis Ebersole - AMATYC Writing Team Member
Northampton Community College, Bethlehem, Pennsylvania
Brian Smith - AMATYC Writing Team Member
Dawson College, Montreal, Quebec, Canada
(Currently at McGill University, Canada)
Francis Merceret - NASA Scientist/Engineer
Kennedy Space Center, Florida
A Cost-Benefit Analysis of the Doppler Radar Wind Profiler at the Kennedy Space Center
Problem Statement
The Doppler Radar Wind Profiler (DRWP) at the Kennedy Space Center (KSC) can detect sudden wind velocity changes that would not be noticed using the traditional method of determining wind velocity changes -- a weather balloon sent aloft one hour before launch. The cost of operating the DRWP is $250,000 per year. With NASA funding being limited, the scientists at KSC need to know whether this expense can be justified. Your mission, should you decide to accept it, is to compare the benefits of using the DRWP with its annual operating cost ($250,000) and to make a recommendation to either stop using the DRWP or to continue funding it. You must justify your recommendation. The DRWP is used for approximately eight Shuttle launches per year and 2 Titan rocket launches per year. Shuttles have a crew of 6 persons while Titan rockets are unmanned.
Mathematical Aside
The benefit associated with the DRWP depends on the value of the Shuttle, the value of a Titan rocket, and the value of the payloads they are carrying. Another factor is the probability that the DRWP will detect a sudden wind velocity change not detectable by traditional means, thus avoiding the destruction of a launch vehicle and its payload. To determine the benefit associated with the DRWP, we need to understand the concept of mathematical expectation. We first introduce several terms.
An experiment is the observation of an occurrence. For example, the Engineers at KSC conducted an experiment when they used the DRWP to record changes in wind velocities over a long period of time. A sample space is the set of all possible outcomes. For the purposes of the KSC experiment the possible outcomes were the possible changes in wind velocity from the last reading made by the weather balloon, so our sample space would be the set of all possible changes in wind velocity. An event is a subset of the sample space. The KSC scientists were interested in the event: “changes in wind velocity with absolute value greater than 20 m/s”, a subset of all the possible outcomes.
Example 1: Consider the following experiment. You will toss a coin and a six-sided die. You are interested in obtaining a head on the coin and either a 5 or 6 on the die. Find the sample space and event.
Solution:
Let S be the name for the sample space. Then S = {(H,1), (H,2), (H,3), (H,4), (H,5), (H,6), (T,1), (T,2), (T,3), (T,4), (T,5), (T,6)} The event E we are interested in is: E = {(H,5), (H,6)}
NASA - AMATYC - NSF
Mathematicians use the concept of mathematical expectation or expected value to indicate the value of an event with different "winnings" and probabilities for each possible outcome. To find the expected value of an event, you must multiply the “winnings” associated with each outcome by the probability of that outcome. The sum of these products is the expected value of the event. In symbols, the expected value V of an event composed of outcomes that have probabilities p 1 , p 2 , p 3 , ... and winnings w 1 , w 2 , w 3 , ... is given by the following formula:
V = w 1 ⋅ p 1 + w 2 ⋅ p 2 + w 3 ⋅ p 3 + ...
Example 2: A fair coin and fair die are tossed. If a head and a 1 or 2 shows, you win $2. If a head and a 3 or 4 shows, you win $5. If a head and a 5 or 6 show, you win $10. Otherwise, you lose $5. What is the mathematical expectation for this game?
Solution: Let p 1 be the probability of getting a head and a 1 or 2, p 2 be the probability of getting a
head and 3 or 4, p 3 be the probability of getting a head and a 5 or 6, and p 4 be the probability of
getting any other outcome. Then p 1 = p 2 = p 3 =
. Also, p 4 =
. The associated winnings are
w 1 = 2, w 2 = 5, w 3 = 10, w 4 = −5. The expected value V is
If you play this game repeatedly, you can expect to win an average of $0.33 per game.
We now have the mathematical tools needed to solve the problem described in the beginning paragraph of this Spinoff. The following four-step model for problem solving will help to guide you through the solution process. Try to remember these five steps, for they can be applied to almost any problem.
What assumptions must you make in order to complete your mission?
State the problem in your own words.
NASA - AMATYC - NSF
Devise a plan State in your own words how you will determine a dollar value for the benefit of using the DRWP.
Carry out the plan Determine the expected value of the DRWP using your assumptions. Use this number to decide whether or not to recommend continued use of the DRWP.
Look back There may be loss of life if the Shuttle is lost. How would this factor affect your recommendation to the KSC Director?
NASA - AMATYC - NSF