All topics Flashcards
slide 1 space weather
What purposes to satellite’s fulfil [4]
- Weather
-Navigation
-Space Physics - Communication
What do planetary Explorers do? [4]
- Fly-bys
-Probes
-Landers
-Rovers
What do Manned Spacecraft do? [3]
-Probes
-Lunar Landers
Stations
Force Equation of two planets
F=MmG/r^2
Spacecraft Angular Momentum
h=r*v=const (both vectors)
Velocity of circular orbit
v=sqrt(mew/r)
period of circular orbit
P=2pi*sqrt(r^3/mew)
Escape velocity
v=sqrt(2mew/r)
Specific energy(kinetic plus temp specific)
e=-mew/2a
velocity for all orbits
sqrt(2mew/r -mew/a)
a for parabolic and hyperbolic
a=infinity a<0
eccentricity [2]
sqrt(1-h^2/(mew*a)) c/a (c is foci and middle)
co planer equation
change in v= 2vi*sin(a/2)
What is the vernal equinox vector?
The vector from the centre of earth to the sun on the spring equinox day. Its a reference system.
Equation for launch site on earth
cos(i)=cos(latitude)sin(azimuth)
What does equation for launch site assume?
Earth doesn’t rotate
Draw out space craft horizon thing find sw,ah,Dh
check in ipad
What is a sidereal day?
a full earth rotation- not counted as an actual day.
What is a solar day?
An actual day, when you’ve turned around enough to face the sun again
What is rotation of Apsides?
Earths pivot point changing each day
What is regression of nodes?
Nodes of an orbit decreasing due to drag
What is a patched conic orbit
A way of getting from one planet to another by orbiting the sun and using hyperbolic orbits
What is C3 in regards to patched conic orbit?
Vhe^2 used to asses energy required for launch of planetary mission
How does Photon propulsion work?
Powerful laser beam directed to provide momentum.
How does Solar sail propulsion work?
Large sheet of film, highly reflective use energy of solar radiation particles
What do Space rockets need that Aircraft engines don’t
oxygen to carry with them
Rocket Equation
v=v0+ vr*ln(m/m-f)
Rocket Equation w/ Impulse
v=v0+Ispgln(m/m-f)
What is Cold Gas propulsion?
Letting pressurised gas out of a nozzle
Why would you use Cold Gas over over propulsion?
Simple
What is Thermal-Solar rockets?
Uses solar energy to increase heat of something
Why would you pick a liquid rocket? [3]
Controllability, Throttling, Restart avalible
What is Throttling?
Changing the Thrust
Why would you pick a solid rocket? [3]
Simple, reliable, quick launch time
What is a hybrid rocket?
solid fuel, liquid oxidiser
What can liquid rocket systems be subdivided into?
Monopropellant and bipropellant
What is monopropellant?
Catalytic decomposition of a single propellant
What is bi propellant
Chemical reaction between fuel and oxidiser
How does Electric thermal work
heat up propellant by passing over a heating element and means it expands and go out fast.
Electrostatic thrusters what they do?
Accelerate positively charged particles in static electric field
Lorentz and Hall what do they do?
Use there own force to move particles to create propulsion
What does nuclear propulsion do?
Some kind of nuclear reaction created heat and therefore pressure
What is Albedo radiation?
Planets reflecting sun radidation
What is predicted temperature range?
results of thermal modelling of the system
What is design operating range?
extremes of predicted temperature range
What is Acceptance temperature range
Limits for operating and non operating modes of a unit
What is a black body?
A material that absorbs all incident radiation
Qualification temperature limit
Flight hardware should be able to operated within these limits to be accepted as part of the satellite (biggest temp limit)
Absorptivity
percentage of incoming radiation that is absorbed by a material
Emissivity
Proportion of radiation emitted by surface compared to a black body at the same temp
Equilibrium Temperature eq
G a A cos(theta) = A omega Eir T^4
Scaling G
G1 * D1^2=G2*D2^2 (unchecked)
What is surface irradiation?
G- total amount of radiation incident upon the surface per unit time and area
What is surface Radiosity?
Total amount of radiation leaving the surface per unit time
What do you assume when doing thermal analysis on real
uniform Temp, constant J, G,a,e across surface.
Equation for net thermal energy leaving a surface
q=(E-J)/(1-e)/eA