1/34
Looks like no tags are added yet.
Name | Mastery | Learn | Test | Matching | Spaced | Call with Kai |
|---|
No analytics yet
Send a link to your students to track their progress
Over expanded
Patm > Pexit
Under expanded
Patm < Pexit
Ideally epanded
Patm = Pexit
Liquid rocket advantage
can throttle, can stop/restart, high Isp
Liquid rocket disadvantage
complex propellant management (liquids are hard to manage in space)
Solid rocket advantage
simple, high thrust to weight ratio (F/W)
Solid rocket disadvantage
can’t restart/stop, can’t throttle
Hybrid rocket advantage
simpler than liquid, safer than solid, can throttle, can stop/restart
Hybrid rocket disadvantage
modest Isp
Isp (specific impulse)
measure of rocket’s efficiency in terms of propellant mass
chemical propulsion (required for launch)
F/W > 1 (150-455 Isp)
nuclear propulsion
political concerns limit use (800-1000 Isp)
electrical propulsion (used only in space)
very low thrust but very efficient (1000-10000 Isp)
2 Advantages of Staging
more total deltaV for same-sized launch vehicle, optimize nozzles for the area it operates in
2 Disadvantages of Staging
increased cost, increased complexity
2 attitude sensors
gyroscope, earth sensor
2 actuators
dampers, thrusters
Is smaller or greater D better for ADCS?
smaller D
Gain
ratio of energy it transmits in its primary direction to the energy that would be available from an omnidirectional source (gain for omnidirectional = 1, directional > 1)
Power
in Watts
Bandwidth
range of frequencies receiver is listening for
Range for worst case
Rmax
Range best case
R = h
three main sources of electrical power
solar, chemical, nuclear
solar (EPS)
only good up to Mars
chemical (EPS)
(ie: battery, fuel cell) primary batteries are only source of power
nuclear
must use past Mars
Depth of discharge (DoD)
% of total stored energy that is removed from battery during discharge period
Heat input in the sun
Solar Input, Albedo, Earth Shine
Heat Input in eclipse
Earth Shine
three methods of heat transfer
radiation, convection, conduction
what method of heat transfer do we use in space and why
radiation because the vacuum makes it the only option
what is fundamental frequency
lowest natural frequency where resonance can occur
resonance
vibrations that increase in amplitude
ideal relationship between f,fund and f,max
f,fund > f,max