L1,L2
L3,L4
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L7
Questions
200

Name TWO assumptions made in projectile motion.

Only force is gravity, gravity is constant, etc. etc.

200

In circular motion:
Direction of centripetal force is ___.

BONUS: Direction of instantaneous velocity is ___.

Radially inwards (or synonym).

BONUS: Tangential (or synonym).

200

Asteroids in circular orbit experience uniform circular motion.
True or False?

True. No tangential forces to vary v_instantaneous.

200

When does K = GMm/(2r)?

When the mass is in circular orbit.

200

Optimal Perm (10^4 kg) unfortunately froze into ice on his way to Technotron, a 10^15 kg planet. Even more unfortunately, he misses it, and starts orbiting at 10^4 m from its centre.
What is the centripetal force on him?

F_c = F_g = GMm/r^2
= (6.67*10^-11) (10^15) (10^4) / (10^4)^2
= 6.67 N 

400

When a projectile is launched, without being on flat ground.
What is the minimum number of given variables required to determine the entire set of flight conditions? (e.g. u, theta, v, h_max, h_init, etc.)

3.

400

Forces accelerate masses to change the direction and magnitude of their velocity.
For forces that stay F ⊥ v, [speed/direction/both] is changed.
For F ∥ v, [speed/direction/both] is changed.

Direction (e.g. centripetal F)
Speed (e.g. tangential F)

400

What happens when an asteroid has F_g = F_c ?

It is in circular orbit.
v_orb = sqrt(GM/r)
etc.

400

Two satellites are orbiting their respective celestial bodies at the same orbital period but different radii.
How is this possible?

r^3 = (GM)/(4pi^2) * T^2
They're orbitting celestial bodies with different masses.

400

The sheriff shots warning shot which travels 1.96km vertically upwards before falling back down and hitting him on the head.
What was its final velocity?

v^2 = u^2 + 2as
v^2 = 0 + 19.6 * 1960 (on the way down)
v = 196 ms^1

600

Describe how vertical and horizontal velocity vary over time, for a projectile.

Vertical velocity decreases linearly from the initial, passing 0 at the max height to reach a negative minimum at impact.
Horizontal velocity is constant at the initial.

600

Explain how changing the width of the screwdriver handle, and length of the screwdriver shaft, affects its effectiveness.

Torque = F_perp * r

Fatter handle = larger r (force arm in plane of rotation)
Longer shaft = no effect (length not in plane of rotation)

600

Compare the orbital velocities and periods of LEOs and GEOs.

v = sqrt(GM/r), i.e. v decr. as r incr.
r^3 = k * T^2, i.e. T incr. as r incr.
LEOs orbit lower than GEOs, so they have higher orbital velocity and lower orbital period.

600

State Kepler's 3 laws.

1. Orbits are elliptical, with the sun at one focus.
2. Satellites sweep out equal sectors in equal time.
3. T^2 proport. r^3.

600

A poorly designed rollercoaster has the minimum required speed to stay in contact to the tracks of a 9.8m high loop de loop.

What is its speed at the top of the loop?

F_net = F_g + N
At top, N=0, therefore F_net = F_c = F_g
mv^2 /r = mg
v = sqrt(gr)
v = sqrt(9.8*9.8) = 9.8ms^-1

800

A 11 y.o. sits at the back of a bus, which is doing circular motion on a roundabout. He tries to hit his sworn nemesis at the front with a paper ball, but his projectile misses because he doesn't account for the bus turning (he's 11).
Describe the ball's motion relative to the bus and ground.

Relative to ground, regular parabolic projectile motion, with bus's intantaneous v added on.
Relative the bus, vertical component of motion same, but on horizontal plane it would appear to have an acceleration that only changes in direction. It would curve to towards the bus wall away from the centre of rotation.

800

List TWO similarities and TWO differences between masses undergoing uniform circular motion on banked tracks and swinging strings.

Similarities
1) v = sqrt(grtanT)
2) F_net = F_x = F_c, i.e. F_y = 0
Differences
1) String: Tension_x supplies F_c,
B. Track: Normal_x supplies F_c
2) B. Track can have friction, giving it a range of v for which any r can be maintained
ETC ETC. 

800

Explain why the direction of escape velocity does not matter, assuming it does not crash into anything.

Gravity only acts on v_rad, where K --> U as a_g reduces v_rad.
Gravity doesn't act on v_tang, hence no work is done on this axis.
But even if v = v_tang initially, the spherical g field means v_tang becomes v_rad as r --> inf.
Hence, the work to escape the field will always eventually be done. 

800

The Broker operates a wrecking ball to destroy the Betmobile, which is driving around a 45deg angled bank track spanning 1960m in diameter.
What is the minimum angular velocity Broker needs to wipe out Betman?

v = sqrt(gr*tanT)
v = sqrt(9.8*980*1)
v = 98ms^-1
w = v/r
w = 98/1960
w = 1/20 = 0.05 rad/s
i.e. need more than 0.05rad/s to work.

1000

Name ALL the other parameters you can derive from t_flight alone, assuming the ground is flat and g=9.8ms^-2.

t_maxheight
u_y
v_y
h_max
(also instantaneous v_y and s_y for any t)

1000

Vertical circular motion, rollercoaster going over top of and under a semicircular hump
how can you determine min/max v given u?
energy --> find v_top = f(u) --> F_c = F_g +- N (N=0) for v_

1000

At the apogee, the moon's F_g is too high to maintain circular orbit with its current v. At the perigee, F_g it's too low.
Explain why satellites will not simply revert to lower/higher circular orbits when v =/= v_orbital, and instead swings elliptically. 

v has radial and tangential components. A circular orbit requires a constant v_tang, and v_rad = 0.
The equation F_c = (mv^2)/r describes the v_tang required for a circular orbit for that r.
Between the apogee and perigee, there is a point where v_tang satisfies what's required for circular orbit, but v_rad = 0 only at apogee and perigee, hence the condition for circular orbit cannot be required.

1000

Millionaire Melon Musk is trying to catch up to Beff Jezos, who launched at v_esc into deep space. He realises that by going beyond v_esc, he can asymptotically approach v_f = 1km/s instead of v_f = 0.
What launch v_i from the Earth's surface does he need to satisfy this whim? (Assume no air res., etc., etc.)

U_inf + K_inf = E_inf = E_surf = U_surf + K_surf
0 + 1/2*mv_f^2 = -GMm/r_E + 1/2*mv_i^2
v_f^2 = -2GM/r_E +v_i^2
v_i = sqrt(v_f^2 + 2GM/r_E)
 = sqrt[1000^2 + 2*(6.67*10^-11)*(6*10^24)/(6.371*10^6)]
 = 11253 m/s
(Notice v_esc is already 11208m/s)