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Space Engineering Institute SEI

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Shows the benefits and efficiency of two-phase flow in active thermal control systems. ... External Active Thermal Control System in use on the International ... – PowerPoint PPT presentation

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Title: Space Engineering Institute SEI


1
Space Engineering Institute (SEI)
Space Engineering Research Center Texas
Engineering Experiment Station, Texas AM
University
Integrated Thermal Energy Management System
(ITEMS)
  • Team Members
  • Christie Tipton, Scott Hansen, Sarah Thiele,
    Nikhil Bhatnagar, Leanne Kristek, Katelyn Lowe
    Jeremy Smith
  • Mentors Dr. C. Kurwitz Dr. K. Hulbert


2
Project Goal
  • The ITEMS concept will demonstrate mass saving
    and energy storage capabilities inherently
    associated with phase change by the isothermal
    sharing of heat between sources and sinks in a
    two-phase thermal management system for
    spacecraft.

3
Project Objectives
  • Build a thermal control system that stores and
    transfers energy using two-phase, isothermal
    fluid.
  • Calculate the ratio of mass of the system to the
    energy handling capability.
  • Compare this ratio to similar single-phase system
  • Shows the benefits and efficiency of two-phase
    flow in active thermal control systems.
  • Conduct a similar evaluation using the ratio of
    power required by the system to energy handling
    capability of the ITEMS loop and existing systems.

4
Fall Semester Plan
  • Research Phase Modeling and Simulation Teams
  • Research single-phase thermal control systems and
    create working models using MØTRAN software.
  • Development Phase Hardware and Instrumentation
    Teams
  • Design and develop demonstration flow loop.
  • Model system using MØTRAN for performance
    prediction under 1g and reduced gravity
    environments.
  • Construct a working two-phase thermal control
    system, demonstrating the ITEMS concept.
  • Set up a DAQ system to monitor the model.
  • Submit a flight proposal to Microgravity
    University.
  • Compare test results of two-phase system to
    analog single phase system.

5
Research Phase Modeling Team
  • Obtained information on
  • External Active Thermal Control System in use on
    the International Space Station.
  • Heat Rejection System used by the Mars Rover
    Spirit during cruise stage.
  • Created data charts of the specifications, and
    developed simplified visual models using
    Microsoft Visio.
  • Used the information gathered about these systems
    when planning the design of our model loop.

6
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7
Research Phase Simulation Team
  • Used data from Modeling Team to create simplified
    MØTRAN models of EATCS and HRS.

8
ITEMS Flow Loop
  • Created a schematic of the ITEMS flow loop.
  • Designed to demonstrate the capabilities of the
    two-phase thermal system.
  • Created a MØTRAN model.
  • Verify the feasibility of our proposed system
    and predict its performance in 1g and 0g
    environments.

9
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10
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11
Development Phase Hardware Team
Vortex Separator
Void Fraction Sensor
Electrical Bay
DP Cell
Ice Bath
Pumps
12
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13
Development Phase Instrumentation Team
  • Calibrated RTD transmitters and pressure gauges
    and began using LABVIEW to interface them with
    the DAQ.
  • LABVIEW allows for efficient data interpretation
    using engineering units in real-time.
  • Provides the ability to program with limited
    programming experience to develop test solutions
    quickly.

14
Spring 2010
  • Goals
  • Finish construction of our test loop and DAQ
    system used to record experimental data.
  • Perform ground testing to evaluate various
    aspects of two-phase thermal bus and to collect
    baseline two-phase data for comparison to MØTRAN
    predictions.
  • Use mass models and specific mass information to
    compare current thermal management systems to a
    similar ITEMS centric design.
  • Publish results.
  • If awarded, perform testing under reduced
    gravity conditions to collect general two-phase
    flow data as well as demonstrate operation of
    ITEMS system in a reduced gravity environment
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