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Radiant Heat Transfer and Homework Discussion

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Phobos Explorer Power System ... orbit around Phobos using 100W continuously ... due to Mars and Phobos combined assume 90 min orbit ( =5g/cc )around Phobos ... – PowerPoint PPT presentation

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Title: Radiant Heat Transfer and Homework Discussion


1
Radiant Heat Transfer and Homework Discussion
  • Lecture 20
  • Space Systems

2
News From Mars
  • Portion of Mars old Ocean found frozen at South
    Pole
  • Enough to cover
  • Mars with 10 meter layer

3
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4
Old Mars Ocean
5
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7
Possible Guitars on Mars
8
Agenda
  • The Blackbody Radiation Curve
  • Thermal Radiation in Space
  • The Cosmic Background
  • Thermal Radiation in Space
  • Homework Problems
  • Attitude control problem
  • Mars eclipse problem

9
Why do the stars shine?
Because they are hot! Including the Sun!
10
Blackbody Radiation Curve
11
Blackbody Radiation Curve
12
Black Body Radiation Curve
13
Blackbody radiation
  • If a body absorbs and radiates EM radiation
    perfectly, it is called a blackbody
  • It then radiates power by the Stefan Boltzman Law
    W/m2 ??T4
  • ?emissivity, 1 for a black body , ? gt1 for real
    surfaces
  • ?5.76x 10 8 Wm 2 K-4
  • ( Stefan-Boltzmann constant)

14
Cosmic Background Radiation
Temperature of space is TCosmos2.72K (cold) (
This is why it is dark at night)
15
Space Thermal Radiation problems
  • Spacecraft receive and radiate heat by blackbody
    radiation
  • They receive radiation because the sun is hotter
    than they are ( 10,000K)
  • They can dump heat to space because it is colder
    than they are (2.7K)
  • These two phenomenon are tools for engineers

16
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20
Homework 4 Solutions
21
Attitude control problem
  • Use the equation for angular momentum
    conservation to calculate the of rotations a
    reaction wheel of 1cm thickness and 10 cm
    diameter and mass 10 grams must turn in order to
    rotate a 1ton 1meter diameter 1meter long
    satellite through 30degrees

22
Attitude control problem
23
Attitude control problem
24
Phobos Explorer Power System
  • How much battery mass at 40Whr/kg , assuming 50
    power margin, for a satellite in tight orbit
    around Phobos using 100W continuously ( assume
    spherical Phobos at 5gm/cc density)
  • Solution Find maximum shadow period due to Mars
    and Phobos combined assume 90 min orbit ( ?5g/cc
    )around Phobos

25
Circular orbital period for tight orbit
Phobos actual density is 2.2g/cc
26
Phobos power problem
R2.76 RMars
Phobos
Period 7.7hr
Mars shadow
Mars
27
Phobos power problem
28
Phobos power problem
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