A proposed interstellar space vehicle comprises an accommodation unit of mass 690 Tons at the front, separated by a light tube between the individual centres of mass, which is 43m. The amount of seperation is necessary to reduce levels (from the nuclear engine) at the accommodation unit. Axes xy are centred on the engine unit centre of mass, with x towards the accomodation unit, and y perpendicular to x. All masses may be considered constant.

Q1 Fund the x coordinates of the centre of mass of the space vehicle.
Q2 The engine operates, giving a thrust of 8.2 MN directly along the connecting tube. Calculate the acceleration, and hence choose one of the following options for the compressive force in the connecting tube.

Q1: To determine the x coordinates of the center of mass of the space vehicle, we need to consider the mass and position of each component.

Given:
Mass of the accommodation unit (m1) = 690 Tons
Separation distance (d) = 43m

To find the x coordinate of the center of mass, we can use the concept of weighted average:

x_cm = (m1 * x1) / (m1)

The x coordinate of the center of mass (x_cm) is the weighted average of the x coordinates of each component, where the weights are the masses of the components.

In this case, since the engine unit is at the origin (0, 0) on the xy axes, the x coordinate of the accommodation unit is the distance between them, which is -43m (negative because it is in the opposite direction).

Substituting the values into the formula:

x_cm = (690 Tons * (-43m)) / (690 Tons)
x_cm = -43m

Therefore, the x coordinate of the center of mass of the space vehicle is -43 meters.

Q2: To calculate the acceleration of the space vehicle, we can use Newton's second law of motion which states that the force acting on an object is equal to the mass of the object multiplied by its acceleration:

F = m * a

Given:
Thrust force (F) = 8.2 MN (meganewtons)

We need to convert the thrust force to newtons, as the mass is given in tons.

1 MN = 1,000,000 N, so 8.2 MN = 8,200,000 N.

We have the thrust force, but we need the mass of the entire space vehicle to calculate the acceleration. The total mass can be calculated by summing the mass of the accommodation unit and the engine unit.

Mass of the accommodation unit (m1) = 690 Tons
Mass of the engine unit (m2) = Given to be constant (not provided)

Total mass (m) = m1 + m2

Since the mass of the engine unit is not provided, we cannot calculate the exact acceleration or compressive force within the connecting tube. Therefore, without the value of m2, we cannot choose one of the options for the compressive force.