This is the remainder of my response, which the Forum wouldn't let me post in one piece:
DaleSpam said:
Sounds good. I will do that, and I predict that his application of Newton's first two laws, including the inertial forces, will correctly describe the motion he observes and that the inertial forces will not satisfy the 3rd law.
So that we can be consistent let's use the following:
mass of the ball = .1 kg
mass of the rocket (including ball) = 1000 kg
mass of the exhaust at t=1 s (if needed) = 1 kg
thrust of the engine = 2000 N
transformation equation between inertial and non-inertial frame: x' = x-t²
ball released gently at t=t'=1s
If I missed something just specify it explicitly.
Okay, let's go through this. I'm not sure I really see the point, since we're just applying the 1st and 2nd laws, which you've already agreed work fine in the accelerated system, but since if you believe the error in my reasoning will be revealed, then on we go ...
Let's define some variables so that the equations aren't just a mash-up of numbers:
mass of ball: [tex]m_b = 0.1 \,\text{kg}[/tex]
mass of rocket (including ball and spaceman): [tex]m_r = 1000.0 \,\text{kg}[/tex]
thrust of rocket motor: [tex]T=2000.0 \,\text{N}[/tex]
We're using primed coordinates, velocities, and accelerations for the accelerating system, unprimed for the inertial system.
I'm going to override your specification that the ball is released at t=1 s (gently - that's good! :-) we don't need any extraneous forces, here!), since there's nothing important happening 1 s before then to start our clocks. I'll just say that t=0 at the moment of release and avoid unnecessary extra terms that look like (t - 1s); if you've gone ahead with your definition, then there will be a lot of "t-1" factors that we can easily correct for.
I'll also say that the origins of both coordinate systems are aligned with the point of release of the ball at t=0, so that point is x = x' = 0 as well.
Then we have initial velocities, all at time t = 0:
rocket initial velocity in accel. stytem: [tex]v'_{r0} = 0\,\text{km/sec}[/tex]
rocket initial velocity in inertial system: [tex]v_{r0} = 10.0 \,\text{km/sec}[/tex]
ball initial velocity in accel. system: [tex]v'_{b0} = 0.1 \,\text{km/sec}[/tex]
ball initial velocity in inertial systme: [tex]v_{b0} = v_{r0} + v'_{b0} = 10.1 \,\text{km/sec}[/tex]
For the acceleration of the rocket in the inertial frame we have:
[tex]a = F/m_r = 2 \,\text{km/sec}^2[/tex]
Next we'll work out the trajectory of the ball in the inertial frame, where we are in agreement about everything.
The position of the rocket (i.e. the origin of the accel. frame) in the inertial frame is
[tex]x_r(t) = v_r t + \frac{1}{2}at^2[/tex]
where [tex]v_r(t) = v_{r0}+at[/tex]
The ball moves inertially once it's released, so its position in the inertial frame is simply
[tex]x_b(t) = v_{b0} t[/tex]
So, what is the distance from the point of release in the rocket (i.e. the spaceman's hand) to the ball at time t? It will be:
[tex]h(t) = x_b - x_r = v_{b0} t - v_r t - \frac{1}{2}at^2 = (v_{b0}-v_r)t - \frac{1}{2}at^2[/tex]
Now let's go to the accelerated frame. The ball is subject to the inertial force in the "downward" direction, so its postion will be:
[tex]x'_b(t) = v'_b t - \frac{1}{2}at^2[/tex]
But we note that since the ball's (constant) velocity in the inertial frame is just
[tex]v_b = v_{b0} = v_r + v'_b[/tex]
we get
[tex]v'_b = v_b - v_r[/tex]
so
[tex]x'_b(t) = (v_{b0}-v_r)t - \frac{1}{2}at^2 = h(t)[/tex]
In other words, by invoking Newton's Laws in his accelerated frame, the spaceman predicts exactly the same answer that we do in our inertial frame.