This paper presents methods of orbit transfer for small planetoids from the main belt to the future colonies on Mars using current technologies. The results show that by using nuclear weapon or even kinetic energy weapon (for retrograde bodies) asteroids with masses up to about 100 tons can be moved. Both options assume that asteroid will survive explosion.
In recent years there is a growing interest in the planetoids, concerning extraction of precious materials from them, like iron, nickel, water or platinum [
The methods we employ are similar to those considered in the case of a deflection of an asteroid on the collision curse with the Earth [3-5].
In Chapter 2 we consider nuclear explosion in front of an asteroid, in Chapter 3 kinetic energy weapon, Chapter 4 considers the effect of light pressure on the asteroids and finally in Chapter 5 we present a short summary.
Let’s consider sending a spacecraft equipped with nuclear weapon to an asteroids. Assuming nuclear explosion just in front of an asteroid (
We treat the interaction between the products of nuclear explosion and an asteroid as an inelastic collision. Supposing proportionality of momentum and energy like
for radiation, from the conservation of momentum follows:
where—velocity of an asteroid before explosion,—velocity of an asteroid after the explosion,— mass of an asteroid.
Hydrogen bomb can release of energytypical asteroids velocity in the main belt is
and the final velocity we want to achieve is according to Hohmann transfer [6,7] between asteroid-Mars system:
Introducing these numbers to the Equation (1) we can compute the mass of the asteroids which can be moved in this way:
If we suppose that an asteroids is built from pure nickel, and current price 18 $/kg the asteroids will be worth more than 1 million dollars.
The similar procedure can also be applied for the Kuiper belt objects.
As a second possibility to move an asteroid we consider shooting an asteroid by 5 tons weapon from the Earth orbit. This approach can be useful if we can find an asteroid which orbit the Sun in the opposite direction as the Earth does (retrograde motion)
In that case we can take advantage from the Earth motion around the Sun (about). For an inelastic col-
lision the conservation of momentum leads to:
where—mass of an asteroid, where—mass of a weapon,—velocity of an asteroid before the collision,—velocity of an asteroid after the collision,—velocity of the weapon.
The velocity of the weapon shot from the Earth in the moment of collision is:
Substituting this and, to the Equation (2) we get:
We can also consider an elastic collision, which is probably more difficult to construct (something like air bags used by NASA in Mars missions). In this case from the conservation of momentum and energy follows:
which after substitution yields to:
The solution of the above equation gives for the mass of the asteroids possible to transfer in this way:
This value is more than twice the mass possible to move through inelastic collision.
As a third possibility for moving asteroid to a desired position let’s consider attaching a huge solar sail. The average force in Newton’s acting on a sail from light pressure at a distance about 2AU is:
where—area of the sail in square meter.
Considering sail with area we get the force about. Depending on the orientation of the sail we can move asteroid spiralling inward or outward from the Sun [
Substituting the mass of the asteroids possible to move in about a year is:
Another option using the pressure of the light which can be considered is to attach small nuclear reactor equipped with a laser to an asteroid. In this scenario the energy generated by nuclear reactions is used to power the laser. The beam of light from the laser is sent in the direction of the velocity of the asteroid. As a result asteroid will spiral from the main belt inward the Sun and can reach the Mars orbit. If the reactor has the mass M and the power 100 MW the mass of the asteroid which can be transferred from the main belt to the Mars in a year is about:
Assuming mass of the reactor with fuel, mass of the asteroid is also.
From the options considered, the most universal is a nuclear blast in front of the asteroid. The biggest possible mass to move from the main belt to Mars we got in elastic collision between missiles ejected from the Earth and an asteroid is 131,000 kg. However this possibility requires finding an asteroid which orbits the Sun in the opposite direction. Both options assume that asteroid will survive explosion (collision). The last options, solar sail for main belt asteroids and nuclear reactor + laser for any asteroid are not destructive and most safe; however allow only moderate masses to transfer.