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MARS LANDER INVESTIGATION Help With Vernier GO Devices is HERE |
BACKGROUND: The atmosphere on Mars is VERY thin... about 100 times *less* dense then the atmosphere of our Earth at Sea Level. It is composed of about 95% carbon dioxide, 2.7% nitrogen, 1.6 percent argon and trace amounts of other elements. As you might expect, trying to parachute a lander onto the surface of Mars is quite an engineering challenge. According to NASA (https://www.nasa.gov/vision/universe/solarsystem/mars_challenges.html), 2 out 3 missions to Mars have failed. Here's how that article summarizes the descent to the surface:
Needless to say, the landing's on Mars are NOT gentle. So... We want to send people to Mars, but we don't want them to experience a "hard" landing. We know that parachutes are only marginally helpful so we have to build some sort of container to keep our passenger safe on impact. INVESTIGATIVE QUESTION: Can we successfully model a final stage descent on the planet Mars using classroom materials? Please consider the following: 0) Parachutes are NOT allowed. Remember, the goal here is to simulate the descent of the probe AFTER it is released from the parachutes described above. 1) You must use the physics principles inherent in impulse to provide measureable data to support your claim that your passenger has survived the landing. The following forumae are common examples of how we describe impulse in physics terms: J = Impulse = F∆t = ∆p or more usually F∆t = ∆p F = dp/dt ∫Fdt = p Where:
Your investigation must provide measurable data to support your claim that your passenger (an egg!) has survived the descent or data that shows why your passenger did not survive the the descent from the top of the sky bridge down to the pavement below. I think it might be fun to have a gentle competition here: The group that has the lander with the LEAST mass AND surviving occupants (READ: unbroken egg) wins! Be thinking about that.... I'll have you folks determine rules and other specifications early next week.
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