RocketSTEM Issue #14 - March 2017 | Page 22

Helo, Mars! Objective Apply trigonometric ratios to the NASA Mars Helicopter Scout so that flight data such as climb angle and average speed can be calculated given initial flight parameters. Vocabulary • Slope: The angle the rille wall makes to the horizontal. • Above Ground Level (AGL): The altitude as measured from the local area. • Altitude: The height that an object is in the air. • Average Speed: The Round Trip Distance divided by the Travel Time Climb. • Angle: The angle formed between the rover and the FTP. • Distance to FTP: The distance from the rover to a point above and downrange of the rover. • Flight Time Capacity: The amount of time that is avail- able to fly. • Fly–To–Point (FTP): A point above the Martian surface. • Ground Distance: The downrange distance from a rover. • Hover Time: The amount of time spent in a stationary position above the ground. • Round Trip Distance: The distance from the rover to the FTP and back to the rover. • Travel Time: The time it takes to fly a certain distance. Narrative Roving on Mars is a great way to get from point A to point B, with scientists back on Earth always looking for For a more in-depth treatment of this high school project by Joe Maness & Rich Holtzin visit www.stemfortheclassroom.org. 20 20 interesting places for the rovers to go visit and analyze. However, sometimes finding the next spot to visit can be a daunting task since scientists have to rely on satellite imagery to find compelling places to visit. But even these satellite images are not that detailed; it follows that a closer inspection of the places is always more desirable. In the same way that a ship on the ocean has a Crow’s Nest where the crew can see further, getting to higher ground allows for greater vision of the rover on Mars. But how on Mars can one get to a higher place to see further? Several solutions present themselves, but each solution is not noteworthy. For example, a tower can be erected from the rover, but the complexity and the mass penalty is probably too much. It would be nice if we could scout the area ahead of the rover, and survey without weigh- ing too much. The reason is because an increase in mass equals to an increase in the amount of propellant need- ed just to get off the ground. Analysis Enter the Mars Helicopter Scout (MHS). This little and ultra light weight flying machine can take off from the rover and fly out to a distance that the rover cannot see. It has solar panels on the top of the machine, and has two counter–rotating rotors that generate lift in the thin Martian air. The best part? The entire helicopter has a mass of only one kilogram! The MHS is activated, and is sent instructions to go to a certain Fly–To–Point (FTP) away and above the rover. The helicopter lifts off and flies to the FTP, hovers, and takes im- ages of the terrain that the rover cannot see. Afterwards, the MHS flies back to the rover where it shuts itself down and uses the solar panels to recharge its batteries. Nice! The MHS has around 3 minutes (180 seconds) of flight time capacity, and has a maximum altitude of 120 www. RocketSTEM .org