ERAST Pathfinder:

Plotting Wind Speed and Altitude


Author: Robin A. Ward, California Polytechnic State University-San Luis Obispo


Audience: grades 7 - 8


Mathematical Topics: graph construction and interpretation


Rationale: The NCTM Standards recommend that the mathematics curriculum for students in grades 5-8 include explorations of real-world statistical data, which would provide students with the opportunity to:

  • construct, read, and interpret tables, charts, and graphs; and
  • draw inferences and develop convincing arguments that are based on data analysis.

    This activity allows students to plot real-world data and search for and discuss the existence of relationships among the data.


    Background: One vital piece of data collected by Pathfinder during its flights is the wind speed at various altitudes. Knowing the wind speed is extremely important to operators on the ground since flight operations are limited to relatively calm wind days. This is because Pathfinder is a very lightweight vehicle, weighing only 530 pounds. For a flight to be stable, the surface wind speed must not exceed 5 knots (approximately 6 miles per hour). As Pathfinder reaches higher altitudes, the surface winds must range between 5 - 7 knots (approximately 6 - 8 miles per hour), with upper level winds less than 50 knots (approximately 75.5 miles per hour). Thus, a constant observation of wind speed is imperative to insure a safe return of Pathfinder to Earth. A knot is a unit of measurement used to measure speed at sea. One knot equals 1 nautical mile per hour or 1.151 statute (or "land") miles per hour.


    The Activity:

  • During a recent mission in August of 1997, Pathfinder collected the following altitude and wind speed data. Share this data with the students.
  • Next, students will observe and discuss any patterns in the data. What happens to the wind speed as the altitude increases? Does the wind speed also increase? Ask one or two students to come to the board to make a raw sketch of what they think the graph of altitude (x-axis) versus wind speed (y-axis) might look like.
  • Using the altitude and wind speed data, students will create a graph displaying altitude (x-axis) versus wind speed (y-axis). Did their graph match any of the original predictions?
  • Students should notice that there is no relationship between altitude and wind speed. That is, if the altitude increases (or decreases), the wind speed does not necessarily increase (or decrease) as well. Thus, the wind speed is independent of altitude. Promote a discussion as to why there is no relationship between wind speed and altitude. Ask students to justify their thinking and reasoning.


    Enrichment: As an enrichment activity, tell students they are actual NASA Dryden engineers called in to assist in the flying of Pathfinder. Place students in groups and let them work cooperatively to design emergency scenarios to handle when winds would exceed the limits of Pathfinder. How would the students change their flight plan?

    Present the following scenario: Due to a communications failure, the entire flight plan for the August 28, 1997 flight of Pathfinder has been deleted. Ask students to pretend to be actual NASA Dryden engineers assigned to reconstruct the flight plan just completed by Pathfinder. The only data the "engineers" have to work with is the wind speed and altitude data given above. Using this data and the graph they just created, showing wind speed (y-axis) versus altitude (x-axis), ask the "NASA Dryden engineers" to develop and present possible flight plans completed by Pathfinder by generating a graph plotting Pathfinder's altitude (y-axis) versus time (x-axis), taking into account the varying wind speeds.

    Students may observe and plot other Pathfinder data that does show a relationship. Allow students to discover the linear relationship between altitude and temperature.

    Students can also engage in another activity that demonstrates a piecewise linear relationship between time and Pathfinder's battery state of charge.


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  • Funded by the NASA Dryden Flight Research Center


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