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Aerobraking

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calculate an orbit from initial conditions -understand the effects of drag ... Two Dimensional Integration. Choose coordinate system -Origin at planet's center ... – PowerPoint PPT presentation

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Title: Aerobraking


1

Aerobraking
Mollie Devoe
Wells College
2
Agenda
  • What is Aerobraking?
  • How Aerobraking works
  • Aerobraking Simulation
  • Results
  • Programs future

3
Setting the Stage
4
What is Aerobraking?
  • Aerobraking is a technique to transform an
    elliptical orbit into a circular orbit
  • Aerobraking exploits a planets atmosphere to
    perform a controlled drag maneuver.

5
How Aerobraking Works
  • Atmospheric molecules strike the spacecraft
    transferring energy and momentum.
  • The momentum transfer creates drag which
    aerobrakes the spacecraft.

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Types of Aerobraking
  • Single-Pass
  • Multi-Pass

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Phase 1 Walk-in
  • Propulsive maneuvers gradually drop the
    spacecrafts periapsis
  • This allows evaluation of the vehicles response
    to the new environment in gradually increasing
    levels

10
Phase 2 Main Phase
  • A series of small propulsive maneuvers keep
    periapsis in control corridor

11
Phase 3 Endgame
  • Desired circular orbit is met
  • Propulsive maneuvers raise periapsis out of
    atmosphere to stop aerobraking

12
Project Goals
  • To understand orbital mechanics
  • -calculate an orbit from initial conditions
  • -understand the effects of drag
  • Build a program that simulates aerobraking

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About the Program
  • Application parameters
  • -planet mass, planet radius, spacecraft mass,
  • time lapse
  • Current position
  • -x, y, r, theta, velocity, net force...
  • Updates current position, including total energy
    and angular momentum

14
Two Dimensional Integration
  • Choose coordinate system
  • -Origin at planets center
  • Position is a function of x and y

15
Velocity at Specific Position
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Therefore the New Position After dt is...
  • In x direction

17
What About the Change in Velocity?
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The New Velocity After dt is...
19
Running the Program
  • Simulations run with the following initial
    velocities
  • - 0 m/s
  • - 1200 m/s
  • - 1250 m/s
  • - 1275 m/s
  • - 1280 m/s
  • - 1300 m/s

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A Closer Look...
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The Programs Future
  • Run more simulations to gain a better
    understanding of drag
  • Three dimensional integration
  • Apply to other planets

29
Acknowledgments
  • Professor Scott Heinekamp
  • Professor Carol Shilepsky
  • Frank Lacomb
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