Lectures 1-15 Flashcards
“Pale Blue Dot” was taken by what spacecraft?
Voyager 1
Earth’s first artificial satellite
Sputnik
Define “bootstrapping”
taking a known, measures quantity, and using it to infer the value of another quantity
How have we known the size and distance of the moon for 2200 years?
Aristarchus of Samos measured the time it took for the moon to pass through Earth’s shadow during an eclipse and compared it to the time it took for the moon to move its own diameter in the sky
What assumptions did Aristarchus of Samos make when measuring the size and distance of the moon?
1) Earth was a sphere
2) the sun is very far away- Earth’s shadow is straight
A star’s parallax is defined by
one-half of the angular shift of the star over the course of a year
One parsec is
the distance equivalent to one arcsecond (1/3600 degrees)
Equation for distance in parsecs is
d=1/p(in arcseconds)
1 parsec= ___ light years
3
What is Gaia?
ESA spacecraft to measure space
What was the Vanguard Project?
American rocket program. Was reinvigorated after the Russian success of Sputnik
What is Newton’s First Law?
A body in motion stays in motion
What is Newton’s Second Law?
F=ma
What is Newton’s Third Law?
For every action, equal and opposite reaction
Newton’s Law of Gravity
F=(Gm1m2)/d^2
Equation for uniform circular motion
F=(m1 v^2)/d
Equation for orbital velocity
sqrt(G M_earth/d)
Energy, or work, is equal to
Force x distance
KE=
.5mv^2
PE=
(GmM_earth)/R_earth
Escape Velocity=
sqrt((2GM_earth)/R_earth)
What was Luna 1
Launched by the USSR in 1959 with the goal of impacting the moon- missed but first spacecraft in heliocentric orbit
What is the Kessler effect
a scenario where the density of objects in LEO is high enough to be the catalyst for generating more collisions, which would create more space debris, which would cause more collisions…
Pros of elliptical orbit
Allows operation further from Earth with close approach for data downlink
Pros of polar orbit
Good orbit for mapping and surveillance
Geostationary orbit is
Orbit that has same rotation speed as Earth
Equations to find geostationary orbit
d^3=(P^2GM_earth)/(4*pi^2)
d includes radius of earth=6400 km
The mass of a typical rocket is about ___ to ___ fuel
80 to 90
Reasons against space elevator:
1) materials too heavy- will snap
2) materials too weak- snap under their own weight (carbon nanotubes?)
3) power supply issue- conventional means will snap under weight (lasers?)
Period of orbit=
2piR(r_earth+altitude)/V_orbit
V_orbit= sqrt(GM/d(altitude+6400 km))