Chapter 3 - Science Flashcards
Test Review for Chapter 3 (20 cards)
Aphelion
The point in a planet’s orbit where it is farthest from the sun
Perihelion
The point in a planet’s orbit where it is closest to the sun
Apogee
The point in a moon’s orbit where it is furthest from the planet
Perigee
The point in a moon’s orbit where it is closest to the planet
Bound orbit
An orbit in which an object orbits another object repeatedly
Unbound orbit
An orbit in which an object passes by another object once and then never again
Eccentricity
How much an orbit deviates from a perfect circle
Escape velocity
The minimum speed needed to escape an object’s gravity from a certain point
Orbital period
How long an object takes to complete one orbit
Semimajor axis
The longer axis of an object’s orbit
Aristotle
Believed that the Earth was the center of the universe and everything else orbited it in perfect circles
Ptolemy
Developed the “circles on circles” model of the universe to explain apparent retrograde motion
Copernicus
Developed a heliocentric model of the universe where the Earth orbited the sun in perfect circles
Galileo
Supported the heliocentric model with observational evidence
Discovered several moons of Jupiter
Isaac Newton
Developed three laws of gravity which describe gravitational forces within the solar system with reasonable accuracy
Johannes Kepler
Used Brahe’s observations to develop three laws of planetary motion
Suggested that planets did not orbit in perfect circles
Tycho Brahe
Made extremely detailed observations of the motion of stars, comets, and planets over many years
What is Kepler’s First Law of Planetary Motion?
Planets orbit the sun in an elliptical orbit with the sun at one focus
What is Kepler’s Second Law of Planetary Motion?
A planet sweeps out equal areas of its orbit in equal times
Application: planets orbit faster when farther from the sun and slower when closer to the sun
What is Kepler’s Third Law of Planetary Motion?
A planet’s orbital period is proportional to the length of its semimajor axis
Orbital period squared = semimajor axis cubed