It would be the temperature of the steel decreases and the temperature of the water increases
Answer:
The expression for the initial speed of the fired projectile is:
![\displaystyle v_0=\frac{M+m}{m}(2gL[1-cos(\theta)]^{\frac{1}{2}})](https://tex.z-dn.net/?f=%5Cdisplaystyle%20v_0%3D%5Cfrac%7BM%2Bm%7D%7Bm%7D%282gL%5B1-cos%28%5Ctheta%29%5D%5E%7B%5Cfrac%7B1%7D%7B2%7D%7D%29)
And the initial speed ratio for the 9.0mm/44-caliber bullet is 1.773.
Explanation:
For the expression for the initial speed of the projectile, we can separate the problem in two phases. The first one is the moment before and after the impact. The second phase is the rising of the ballistic pendulum.
First Phase: Impact
In the process of the impact, the net external forces acting in the system bullet-pendulum are null. Therefore the linear momentum remains even (Conservation of linear momentum). This means:
(1)
Second Phase: pendular movement
After the impact, there isn't any non-conservative force doing work in al the process. Therefore the mechanical energy remains constant (Conservation Of Mechanical Energy). Therefore:
(2)
The height of the pendulum respect L and θ is:
(3)
Using equations (1),(2) and (3):
(4)
The initial speed ratio for the 9.0mm/44-caliber bullet is obtained using equation (4):

Answer:
1) D
Explanation:
You have to use a consistent air speed to play the trumpet correctly
<span>The payload will continue in orbit along with the space shuttle and their relative velocities will be close to zero. However, depending up the relative orientation of the space shuttle's center of mass and the payload's center of mass, the orbits of both the shuttle and payload is likely to slowly diverge from each other. To illustrate how low the relative velocities would be, let's assume a near worse case situation happens and the center of mass of the payload and the space shuttle differs after the release by 50 meters, then the resulting orbital periods of the shuttle and the released payload would differ by about 0.06 seconds from each other.</span>