Methods of propulsion
Chemical
Ion
Solar
More fanciful:
Warp Drive
Quantum Drive
Newtons Laws
First: Inertia
Second: F = ma
Third: Law of opposite
LEO
Low Earth Orbit:
The Kessler Syndrome
The Kessler effect
The increase in density of objects in LEO, due to space position is high enough that collision between objects could cause a cascade (cause further collisions)
MEO
Medium Earth Orbit:
Van Allen Radiation Belts
Collection of charged particles emanating from the sun and carried by the solar wind
Communications and GPS satellites use this region as it encompasses an orbital period of 12 hours
GSO
Geosynchronous Orbit:
GEO
Clarke Orbit or Geostationary Earth Orbit:
HEO
High Earth Orbit:
Periods of Orbit
The orbital periods depend upon the major axis of the orbital ellipse and the mass
P^2 = 4pi^2 a^3 / G M2
Escape Velocity
For a satellite to escape from the gravitational fields of the Earth must reach escape velocity
Vsec = root (2GM/R)
Chemical Rocket Fuel
Combustion
An oxidizer is important since there is no air in space
Liquid fuel can be stopped and started potentially many times
Solid rocket fuel can not be stopped when ignited
Chemical fuel parts
Liquid Oxidizer is always liquid oxygen
Liquid fuel can be hydrogen (commonly) or Kerosene (RP - 1)
Ion Propulsion
Chemical rocket propulsion is essential for lifting a rocket
Ion engines produce low thrust and thus low acceleration
Same for chemical rocket propulsion
How does Ion propulsion work
Step 1: Electrons are remitted by the discharge hollow cathode, traverse the disc charge chamber, and are collected by the anode walls
step 2:propellant is injected from the plenum and travels towards the discharge cathode
Step 3: Electrons impact the propellant atoms to create ions
Step 4: Ions are pulled out of the discharge chamber by the ion optics
Step 5: Electrons are injected into the beam for neutralization
Ion propulsion used in spacecraft
Dawn spacecraft
Lunar Gateway
Solar sailing
Arthur C. Clarke’s science fiction
Deployment of a large area, low mass “Solar sail”
Use the pressure of sunlight to change speed and direction
Acceleration generated is very small
Matter - Anti-Matter propulsion
When matter comes into contact with any matter, complete and spontaneous annihilation occurs
It offers 100% conversion of matter into energy
we can produce some anti-matter particles but strong them is the challenge
Nuclear powered rocket
Nuclear thermal rocket
The nuclear fission reactor heats and vaporizes the liquid hydrogen and generates thrust
Relatively low but long-term thrust
Concerns include safety of the environment during a lunch failure
Power for spacecraft
Power comes from solar panels that convert sunlight into electricity
Most efficient when close to the sun
Radioisotopes thermoelectric generators
RTG:
Any radiation emitted must be easily absorbed so it wont impact the rest of the spacecraft
Only 3 isotopes are commonly used:
Exploring our solar system
Artemis project plans on return to the moon
A human mission to Mars in the 2030s
Human settlements through our solar system are likey within this century
Artemis 1
Launched 2022
To the moon and back (uncrewed)
25 days
Artemis 2
Proposed launch 2025
To the moon and back with a crew of 4
~10 Days