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Designing an airplane
that can fly on Mars!
First we put a rover on Mars, then a
helicopter (Ingenuity). But what about airplanes? This study describes the
design of special wings that will help airplanes fly in the thin Martian
atmosphere
Until recently, no attempt has been made to
fly an aircraft in the Martian atmosphere. On Mars, in fact, the air is much
thinner than on Earth. This means that the air pressure is less than 1% of
Earth’s. So, the main source of hesitation for engineers was whether there could
be sufficient lift. Now we have the answer.
A study published in June 2020 by Oliviu
Şugar-Gabor and Andreea Koreanschi from the University of Salford in the UK
analyzed a possible shape for the cross section of a wing (technically called
airfoil) that would be suitable for flight at speeds close to the speed of sound
(high subsonic) in the Martian atmosphere. On July 30, 2020, NASA’s Perseverance
mission launched to Mars carrying a small helicopter, Ingenuity, the first
aircraft that will attempt controlled flight in the Martian atmosphere using a
pair of rotors mounted one above the other and sharing the same axis of
rotation.
Perseverence and Ingenuity
On Ingenuity, the rotor blades are much
larger and spin much faster than what would be required on Earth, in order to
compensate for the low-density, low-temperature, CO2-based atmosphere of Mars.
The larger blades will generate enough lift to get the helicopter to take off
and remain in flight. However, achieving fixed-wing (airplane-like) flight in
this environment is a challenging problem. These conditions require very high
speeds in order to achieve sufficient lift on the wings.
The team used the SU2 flow solver – a
state-of-the-art software that solves aerodynamics equations in order to study
the behavior of a fluid around a certain shape – to determine the most suitable
airfoil shapes for a low-altitude flight near the equator of Mars. They
considered a fixed value for the lift coefficient – a number that represents the
lifting force on the wings – and they chose it high enough to be sure that
flight is possible. They also considered a range of Mach numbers that represent
the speeds that the aircraft would need to reach. These numbers were 0.66, 0.68
and 0.70 Mach) in order to fly. (For reference, a Mach value of 1 is the speed
of sound and is approximately 767 miles per hour.)
As it results, the optimal airfoil shape
for 0.66 and 0.68 Mach is one with a flat lower surface, a continuously curving
upper surface and a maximum thickness in the middle. For 0.70 Mach, the maximum
camber location (the point where it is more curved) is shifted backwards. This
design is adequate to make so that air particles follow smooth paths on the
upper surface of the airfoil, and at a high speed, in order to avoid the
formation of a chaotic flow.
These results were obtained with a
computational method, but a further experimental work will be necessary to see
if it works in real life. For example, something similar to a Mars flight can be
achieved at a very high altitude on Earth, at least 30,000 meters (about 98,000
feet) above the ground, by using a model smaller than the Martian aircraft being
considered. At this altitude, in fact, the atmospheric conditions are very
similar to those on Mars.
Developing a piloted Mars aircraft is a
long-term goal for a future human settlement on the Red Planet. In fact, smaller
aircraft models could be helpful to provide measurements and observations over
large areas, such as those that can be hard to reach by foot or by rover.
Scientists have sent rovers to Mars throughout the history of space exploration,
and it is now time to soar higher.
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