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Compact Thermal Energy Storage Unit for Next Generation Reusable Launch Vehicles

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Title: Compact Thermal Energy Storage Unit for Next Generation Reusable Launch Vehicles


1
Compact Thermal Energy Storage Unit for Next
Generation Reusable Launch Vehicles
  • Shavonne Ford and G. D. Wesson

Department of Chemical Engineering Florida AM
University/Florida State University
Presented at College of Engineering
Tallahassee, FL August 3, 2001
2
Outline
  • Motivation
  • Background
  • Problem Statement
  • Future Work

3
Motivation
  • NASA Space shuttle
  • Cooling system for the hydraulic fluid
  • Ascending Descending Flight
  • Time restriction
  • Weight restriction
  • Current system
  • Water spray boiler system 210ºF
  • Overheating causes the shuttle to lose
    maneuvering capabilities
  • New system requires a lower temperature
  • Requires a turn around service

4
  • Thermal heat storage systems
  • Heat of reaction
  • Latent heat
  • More compact
  • Constant temperature operation
  • Heat exchanger integrated
  • Optimize heat transfer area by using fins
  • Reduces charging/discharging cycles
  • Sensible heat

5
Thermal Energy Equation
  • Assumptions
  • Constant pressure
  • Constant density
  • Neglect work by viscous forces
  • Fluid at rest
  • Heat transfer due to conduction

Rate of Heat added by conduction
Rate Of accumulation
Rate of work done by pressure forces
Rate of work done by viscous dissipation
6
  • Fouriers Law of Heat Conduction
  • Unsteady Heat Conduction Equation

7
Unsteady Heat Conduction Equation
  • Part I Problem with single phase
  • Part II Problem including phase change
    (Stefan Problem)

8
Problem Statement
  • Investigate the heat transfer process around a
    finned tube
  • Finned tube enclosed by and external cylinder

9
  • Cylindrical Coordinate system
  • 2 D system
  • Thermal conductivity depends on position

10
Simulation
  • Numerically solved using Matlab
  • Finite difference method explicit form
  • Show surface plot w/label
  • Talk about initial condition
  • high temp to lower

11
Future Work - Stefan Problem
  • Investigate the solidification process around a
    finned tube
  • Mode of heat transfer conduction only
  • 3-D system
  • Heat Capacity depends on Temperature
  • Thermal conductivity depends on position and
    temperature

12
  • More than one phase
  • Moving interface
  • Enthalpy method
  • No need to track the interface
  • Valid for entire domain
  • Solid, liquid and interface
  • Easy to introduce the mushy region
  • Numerically solve using Matlab
  • Finite difference method and the enthalpy method
  • Comparison with literature values

13
  • Thermal conductivity depends on temperature
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