1990. Reaching Mars by sailboat
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Appointment on Mars
Taken from the 1990 Journal of Sailing, Year 16, No. 04, May, pp. 46-51.
When it was still science fiction to land the first man on Mars, a group of visionaries in 1990 launched the challenge of the Space Sail Cup, the first space sailing regatta. It was serious, fascinating, with an Italian competitor. A project less crazy than it sounds.
The challenge of the first Space Sail Cup, the first space sailing regatta, which will kick off in 1992, has been launched. Enrolled in this incredible “regatta” are only spacecraft capable of moving by harnessing the solar wind. As the destination, the planet Mars over 400 million kilometers from
The news is now known to everyone, thanks to the great prominence given to it by the daily press: theAeritalia, an Italian aerospace company controlled by the Iri Finmeccanica group, has won the selection among European challengers and will represent our continent in the “Columbus 500 Space Sail Cup.” As precisely the name implies, it is a real space
The solar wind
It is necessary to clarify one thing at once: the “solar wind”, that is, the flow of high-speed protons and electrons emitted by the Sun and cited by several not-very-well-informed sources as the propeller of the “solar sail,” actually plays a minimal role: in fact, its thrust is 1,000 to 10,000 times less than that produced by light. Instead, it is precisely the light emitted by the Sun that will “blow” , very feebly when compared to the Earth’s wind, on the sails of the Space Sail Cup participants. Unfortunately, the concepts of quantum mechanics, which are used to understand the interactions between sunlight and sail, are not so easy to explain. And indeed, there must be a reason why a fellow named Albert Einstein won a Nobel Prize on these theories! Among other things, he established the principle of equivalence between mass and energy, expressing it with the well-known formula
The race course and tactics
We can distinguish the path of the spacecraft into 3 basic stages:
1) in the first phase, the goal is to reach lunar orbit–the first “buoy” of the race–in the shortest possible time and pass as close to our satellite as possible, partly to take advantage of its gravitational field for propulsive purposes.
2) the immediate next goal will be to place the spacecraft into interplanetary orbit around the Sun, thereby disengaging it from Earth’s gravitational field.
3) The third phase will be the actual navigation to Mars.
Phases 1 and 2 are undoubtedly the most critical, as the spacecraft will be orbiting the Earth and will have to increase its rotational speed by ensuring that the thrust imparted by the sail is the maximum possible along the route. To do this will require continual maneuvering of the sail, which will come to be in some sections “against the sun” and in others with the “Sun aft” (see Figure 2). This will require sophisticated and continuous trim control, to allow the sail to be in a condition of maximum useful thrust at all times (see figure 3). Phase 3, on the other hand, will be possible to accomplish with 2 different “‘tactics.” A first tactic, which is simpler because it does not require attitude adjustments, is of the same type as that implemented to reach the Moon. This time, however, as the ship’s rotation is directly around the sun, the sail trim will be constant and such as to maximize total energy storage. With this tactic it is planned to reach Mars in about 4.8 years, describing the “spiral” (see Figure 4). The second possible tactic starts from the physical assumption that an elliptical orbit has the same energy content as a circular orbit having a radius equal to the semi-major axis of the ellipse itself. It is therefore possible, by following an elliptical orbit, to reach a single point in the orbit of Mars with less energy than that required by the first tactic. In this way, Mars could be reached in “only” 3.5 years (see figure 5), with consistent related difficulties, however, due to: the need to continuously adjust the sail to make the ship’s orbit elliptical around the Sun; and the navigational precision required to find oneself at the rendezvous with Mars at a very precise point in its orbit (see figure 6).
Aeritalia Project to “sail” to Mars
Why the name of “Capitana Italica”. Capitana was the first name of
The sail – Constructed of 5-micron-thick Mylar and subjected to an “aluminization” treatment on the 2 faces to increase its reflective power, it has a surface area of 10,000 square meters. Its shape is square with a side of 100 meters. In order to make it possible to stow the entire spacecraft inside a standard container transportable by the Shuttle or an Ariane rocket, it was necessary to devise a very “daring” structure capable of unfolding itself once launched from the carrier. The idea is both very simple and ingenious: 4 inflatable spars hinged to the center of the sail and arranged according to the diagonals of the sail itself. These spars are real inflatable “tubes” like those of pneumatic dinghies, made of Kevlar fabric pre-impregnated with a special resin that can polymerize by the heat of the sun and the catalyst contained in the inflation gas. The sequence of sail opening is rap- presented in its four main stages on the opposite page. The total weight of the sail and support spars is only 126 kg! To make the most experienced sailmaker envious.
The mast-It consists of a carbon-fiber lattice structure that can extend telescopically and reach the operational length of about 10 meters.
The ship – It is the “brain” of the system. It contains the on-board computers, telecommunications equipment, facilities for scientific experiments, solar panels for generating the electricity needed to power the satellite services, and sail controllers.

by Paul Damia
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