One more thing, with this 8marker from 2010, I have absolutely no idea how to approach it, if you guys could perhaps give a dot point outline (or if you have time, a response ) on what I'm supposed to cover, that would be absolutely amazing!
Two significant problems that will affect a manned spaceflight to Mars are:
-the changes in gravitational energy
-protecting the space vehicle from high-speed electrically charged particles from the Sun
Use your understanding of physics to analyse each of these problems.
Thankfully this isn't in the 2016 paper otherwise it would be 8 marks out the window! Rip
Neutron
Hi, I'll try answer this the best I can, splitting the question into 2 parts for 4 marks each.
Changes in gravitational energy
- Gravitational potential energy is defined as -GmM/R, therefore as the rocket LEAVES Earth, it's gravitational energy increases. However, the law of conservation of energy (dictating that the total energy in a closed system is constant), suggests that energy must come from another source. This other source is the Kinetic energy / chemical energy within the fuel of the rocket. As the rocket leaves Earth, the KE of the rocket decreases (increasing GPE). This is a problem. In order to maintain the level of KE and increase the velocity of the rocket, more fuel must be burnt and used up. This involves the firing of rocket boosters to provide a constant thrust for the rocket.
- When the rocket enters the G field of Mars, the reverse situation happens. It begins to accelerate, being attracted by the gravity of the planet, towards the surface. As a result of its acceleration, it converts GPE to KE very quickly, losing altitude but gaining heat (from friction) and velocity. (Law of conservation of energy). This again is a problem as a velocity too high is difficult to control, and may be fatal for the probe/occupants inside. In order to solve this problem, rocket boosters are fired in the opposite direction to slow the descent of the probe, reducing its KE as it's GPE decreases.
High Speed Electrical charged Particles
- High speed electrically charged particles coming from the sun are often come from solar flares (where the sun emits a burst of solar radiation). They are quite problematic as they can damage sensitive equipment within the spacecraft and also penetrate through the walls of the spacecraft, damaging other parts inside and may be harmful for the occupants. Alongside causing damage, these charged particles interfere with communication (much like the situation of an ionisation blackout in re-entry), which is another problem.
- In order to solve this problem, the outer layer of the spacecraft can be coated with a material which can be electrically charged to repel these high speed charged particles. Insulating material which prevents these particles from penetrating into the spacecraft can also be applied. Furthermore, communication signals can be sent from the backend or the spacecraft (or whichever end isn't being exposed to these high speed charged particles).
I hope thats enough to get 7 marks at least haha but that's my attempt