Exam 1 Flashcards

1
Q

Kepler’s Laws

A
  1. orbits are either elliptical or hyperbolic
  2. the speed of an orbiting body is fastest at periapsis and slowest at apoapsis
  3. the larger an orbit’s major axis, the longer the orbital period
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2
Q

In what special position in the Earth’s orbit is the Sun?

A

The Sun is at the OCCUPIED FOCUS of the Earth’s orbit. The Perihelion and Aphelion are not points IN the orbit, they are points ON the orbit.

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3
Q

In an elliptical orbit around the Earth, which point has the maximum energy of position?

A

The highest EOP is at apogee, because the EOP increases as you get further, like a roller coaster.

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4
Q

What causes the seasons on Earth?

A

The seasons are caused by Earth’s axial tilt. Eccentricity, in this case, doesn’t matter, because the Earth’s orbit is fairly circular.

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5
Q

During a journey from Earth to Mercury, how are you moving with respect to the Sun?

A

You are speeding up with respect to the Sun. During most of the journey, you’re orbiting the Sun, in order to fall from the aphelion of your transfer orbit to the perihelion of your new orbit.

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6
Q

If you are orbiting the Sun and you fire your engines to speed up at perihelion, what happens?

A

Your aphelion increases, and your perihelion stays the same. Whatever point on the orbit you make the change will stay the same, but the opposite point will change.

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7
Q

During a launch, which kinds of energy are created by the combustion of fuel?

A

Heat, energy of position, energy of motion, light, and sound.

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8
Q

Which forces are most important in the first few seconds after liftoff?

A

Thrust and gravity/weight are important at first. Drag doesn’t matter yet, but will matter later on. At first, the ship is moving too slowly for drag to matter.

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9
Q

If you’re orbiting the Earth every two hours and you make a maneuver that increases your orbital speed, is your new orbital period longer or shorter than two hours?

A

Kepler’s Third Law.

It’ll be longer than two hours. You’re moving into a larger orbit, meaning it has a longer orbital period.

If you want to travel faster (shorter orbital period) then you want to slow down and fall into an orbit with a smaller major axis.

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10
Q

If you’re traveling in a circular orbit around Earth at 7.8 km/sec, what would happen if you slowed down to 7.7 km/sec?

A

Normally, you’d fall into a lower and smaller elliptical orbit.

But, because 7.8 km/sec is the MINIMUM speed required to be in the LOWEST POSSIBLE Earth orbit, slowing down would cause you to become suborbital and the perigee of your new orbit would be inside of the planet.

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11
Q

If you’re in an elliptical orbit around the Earth at 11 km/sec and you increase your speed to 12 km/sec at perigee, what will happen?

A

Normally, speeding up would get you into a larger elliptical orbit with higher perigee, but in this case, you’d hit ESCAPE SPEED and go HYPERBOLIC. A hyperbolic orbit has a perigee, but no apogee.

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12
Q

At what point during a launch do you experience maximum acceleration?

A

You experience maximum acceleration just before burnout.

As you go up, you are losing mass (fuel is being burned), so the ship becomes lighter.

Because it is lighter, the engines are able to push it faster, so it makes you feel heavy and you experience the most acceleration.

Once the fuel is all burned out, you feel weightless. The engines shut off and you float.

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13
Q

The period of the Earth-to-Mars Hohmann transfer orbit is 16 months. So how long will it take to get to Mars via a Hohmann transfer orbit?

A

It’ll take 8 months. It wouldn’t take 16 months because that’s the whole Hohmann orbit, so you’d just end up where you started. But if you travel 8 months, that’s half of an orbit, so then you hit aphelion at Mars.

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14
Q

If you’re millions of kilometers away from any moon, planet, asteroid, or comet, are you orbiting anything?

A

Yes. As long as you’re in the solar system, you’re orbiting the Sun. It’s massive and has very strong gravitational influence.

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15
Q

For most of the journey from Earth to Jupiter, you measure your velocity with respect to what?

A

You always use the center of whatever you’re orbiting at your point of reference, so in this case, because you’re in the solar system and not orbiting a planet or moon, you’d measure your velocity with relation to the sun.

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16
Q

Benefits of various fuel types:

A

Kerosene: cheapest

Liquid hydrogen: cleanest

Solid propellant: highest thrust

Hydrazene: no need for ignition

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17
Q

Why is it good to launch from Florida?

A

Earth spins east, so you get help from the spin.

That sends you over the Atlantic Ocean, where you don’t have to worry about flying over inhabited land.

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18
Q

What is Pitch?

A

X-axis rotation. Pointing the nose up or down.

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19
Q

What is Roll?

A

Y-axis rotation. Spinning along the ship’s length.

20
Q

What is Yaw?

A

Z-axis rotation. Turning nose from side to side.

21
Q

A rocket can only take off if its ___ is greater than the combination of its ____ and its ____.

A

A rocket can only take off if its thrust is greater than the combination of its weight and its drag.

22
Q

What is special about the Space-X Falcon Heavy?

A

It could lift as much weight as any rocket since the Apollo program.

It was able to send multiple stages back to Earth for reuse.

It was built by Space-X, a private company.

23
Q

What did the Falcon Heavy eject into space?

A

The Falcon Heavy ejected a Tesla Roadster. It went into orbit around the Sun, where it will be for billions of years.

24
Q

What is 1 AU from Earth?

A

The Sun, and sometimes Mars.

25
Q

A planet that is cold for 90% of the year and hot for 10% of the year has ______ and ______.

A

A planet that is cold for 90% of the year and hot for 10% of the year has a large major axis and high eccentricity.

26
Q

What’s cheapest: landing, going into orbit, or doing a fly-by?

A

Fly-by.

Going into orbit requires fuel for speeding up or slowing down.

Landing requires a TON of fuel for slowing down.

A fly-by doesn’t require any additional fuel burning.

27
Q

Earth takes 365 days to orbit the Sun. Mercury takes 88 days. Roughly how long is the orbital period of an Earth-to-Mercury Hohmann Orbit?

A

About 200 days.

A Hohmann orbit is in between orbit A and orbit B, so its orbital period is about midway between those of A and B.

200 is roughly in between 88 and 365.

28
Q

You leave an eastward Earth orbit and are heading to Venus. When you make the maneuver to change orbit and head into a bigger one, what time should it be on Earth below?

A

Noon.

Leave for Venus at noon, and leave for Mars at midnight.

This is because, if you leave at noon, you can speed away from Earth whilst slowing down with relation to the sun, so this way you can fall into Venus’ orbit.

29
Q

What can a gravity assist maneuver let you do? What was the first gravity assist maneuver?

A

Slow down, speed up, or change direction.

The first gravity assist maneuver was the Mariner 10 probe, which used Venus to slow down and get closer to the sun in order to reach Mercury.

30
Q

If you’re going from Earth to Mars, why not leave Earth when Mars is at its closest point?

A

This would require too much energy. First, you’d have to leave Earth, then you’d have to hard stop the orbit around the sun and go straight toward Mars.

It makes more sense to fling the craft away from Earth using slightly more velocity than Earth’s orbital velocity, and then catch Mars at the other side of the Sun at the aphelion of the transfer orbit.

31
Q

Why do we launch vertically from Earth?

A

It’s not to overcome gravity quickly, because that’s quite the opposite effect.

Instead, it is to get out of the atmospheric drag in the lowest and thickest part of the atmosphere. This makes the drag much less bad.

32
Q

What’s the more expensive way of getting payloads into orbit: reusable rockets or expendable rockets?

A

Reusable rockets are much more expensive. They have to keep their engines and fuel reserves in order to return, so a lot of their weight is occupied by these things.

In contrast, expendable rockets can lose their engines and fuel, so that leaves a lot of extra space to be occupied by payload.

33
Q

Why was the Space Shuttle unique?

A

Not because it traveled to the moon – it didn’t.

Not because it landed vertically on Earth – it didn’t.

And not because it hit multiple space stations along its route. Other ships have done this too.

It’s special because it was the only aircraft to take people into orbits using reusable engines.

34
Q

What’s the advantage of multiple stage launch vehicles?

A

Despite being expensive and hard to reuse, they’re good because they let you go into orbit using conventional fuels. We still don’t know how to hit orbit without multiple staging.

35
Q

What are some benefits of landing a rocket vertically?

A

It’s cheap to retrieve, unlike an ocean splashdown.

There’s no need for a runway, so you have more options for a landing site.

No need for wings, which are heavy, so you have more room for payload.

36
Q

90% of the mass of a launch vehicle is taken up by the ____

A

Propellant (fuel + oxidizer).

You need a lot of propellant in order to get sufficient thrust to leave Earth’s gravity.

37
Q

What’s special about the following launch types?

Sea Launch
Pegasus Launch
Delta Clipper
Falcon
Venture Star
A

Sea Launch launches from the equator.

Pegasus Launch launches horizontally from an airplane.

Delta Clipper lands vertically.

Falcon lands vertically.

Venture Star uses new nozzle design.

38
Q

What two companies are offering space tourism?

A

Virgin Galactic (owned by Richard Branson)

Blue Origin (owned by Jeff Bezos)

39
Q

What are some advantages of RADAR satellites over photoreconnaissance satellites?

A

RADAR can penetrate clouds.

RADAR can launch to the east.

RADAR can get images at night.

40
Q

What kind of orbits are used by photoreconnaissance satellites?

A

Photoreconnaissance satellites follow retrograde orbits, meaning they orbit around Earth to the west, opposite to Earth’s rotation.

They have to launch toward the west, so they require more push to get into orbit. They work best in sun-synchronous orbits, because then they can take pictures at the same time each day.

41
Q

How long is a solar day?

A

A solar day is 24 hours.

42
Q

How long is Earth’s rotation period?

A

Earth’s rotation period is 23 hours and 56 minutes.

43
Q

Why are communication satellites usually put into the Clarke Band (geostationary)?

A

They are very far away and don’t work on the poles because they are equatorial, but because they orbit Earth at the same rate at Earth’s rotation, they are able to appear stationary from Earth.

44
Q

Which country always launches satellites into retrograde orbits?

A

Israel always launches satellites into retrograde orbits because it usually launches photoreconnaissance satellites which need to be in retrograde orbits.

45
Q

What are Molniya satellites?

A

They are satellites with high eccentricity and high orbital inclination. Usually used for satellite communication in the Arctic.

46
Q

Where can you see a geostationary satellite?

A

They’re very high up, so basically anywhere. Just not the poles (Arctic or Antarctic).