22'033 Mission to Mars Design Presentation - PowerPoint PPT Presentation

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22'033 Mission to Mars Design Presentation

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Title: 22'033 Mission to Mars Design Presentation


1
Survey of Space Nuclear Power Options
2
Dr. Andrew Kadak And Peter Yarsky MIT 12.11.03
3
Introduction
  • The goal of current work at MIT is to identify
    potential Power Conversion Options with use of an
    Ultra High Power Density Core (UHPDC) that will
    be scalable to achieve requirements for a
    plethora of exploration missions, eventually
    meeting the needs for a manned mission to Mars

4
The MIT - UHPDC
  • Ultra High Power Density Core
  • Fast spectrum
  • Tightly coupled / leakage controlled
  • Reactor Grade Plutonium (PuC)
  • 60 Pu239 / 20 Pu240
  • Honey Comb Fuel Nb cladding
  • 20 cm x 20 cm x 20 cm
  • 10 11 MWth (liquid metal)

5
UHPDC Core Layout
6
Outline
  • Power Conversion
  • Thermophotovoltaics (st)
  • Thermionics (st)
  • Brayton Cycle (dy)
  • Rankine Cycle (dy)

7
Thermophotovoltaics (TPV)
  • LM transfers the heat from the core to the
    internal radiator
  • All power is radiated towards TPV collector
  • TPV collectors generate DC from thermal radiation
  • Unconverted heat is dissipated via the external
    radiator

8
TPV Challenges
  • TPV efficiency decreases with higher cell
    temperature
  • The temperature of external radiator is the
    coldest the TPV cells can be (900 K)
  • It is unlikely that TPV Power Conversion will be
    scalable.

9
Thermionic Converters (TIC)
  • TIC Benefits
  • Single or Dual Layered Concepts
  • Static and Direct
  • 12-15 efficiency for TH 1200 K
  • 25 or higher efficiency for TH 2200 K
  • Temperature of heat rejection is 750 K
  • TIC Challenges
  • Direct Contact with the Fuel

10
Conceptual Unit Cell
11
TIC Comparison
  • Low Temperature Single
  • 1200 K emitter / 750 K collector
  • 12 efficiency / 400 kWe
  • High Temperature Dual
  • 2200 K emitter / 750 K collector
  • 25 efficiency / 900 kWe
  • High Temperature Single
  • 2200 K emitter / 1200 K collector
  • 12 efficiency / 2500 kWe

12
Argon Brayton Cycle
13
Comparisons
14
Sodium Rankine Cycle
  • Sodium because
  • 2100 R (1167 K) saturation temperature at 15.4
    psia (1.05 atm)
  • Neutronic Inertness
  • Heat Removal Properties (UHPDC)
  • Saturation Curves are steep (scalability)
  • Little Pumping Power Required
  • Phase Transition (maximal radiator usage)

15
Results for 1200 K
16
Comparisons
17
Conclusions
  • Dynamic PCU technology is more effective and
    scalable than Static (Sodium Rankine in
    particular)
  • Static direct energy conversion is still
    attractive from a reliability standpoint (TIC in
    particular)

18
BONUS SLIDES
  • Slides in case we need clarification

19
Single Layer Concept
  • LM flows through UHPDC
  • LM heats the emitter
  • Electrons flow towards collector
  • Collector is in direct contact with external
    radiator

20
HEU alternative
  • Less Reactive Fuel
  • Larger Core
  • More Fuel Mass
  • More shielding Required
  • No Fertile-Fissile Species (240Pu)
  • Larger Reactivity Swing
  • More demand on Control Devices
  • Work Still in Progress on CBA
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