1. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Representative response to state variation and continuous thermal state averaging heat dissipation schemes Figure Legend:

2. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 The EMU and one constant temperature radiator integration concept. (Space suit image credit: NASA). Integration scheme modified from Ref. [13]. Figure Legend:

3. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Mechanical counter pressure suit concept and constant flux concept. Space suit image credit: Professor Dava Newman, MIT. (Used with permission–Illustration: Cam Brensinger.) Integration scheme modified from Ref. [13]. Figure Legend:

4. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Example of intermediate emissivity settings achieved with a variable potential source Figure Legend:

5. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Example of effective net emissivity values achieved by high–low state mixing Figure Legend:

6. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Space suit radiator surface area scaled to a cylinder approximation Figure Legend:

7. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Cylinder area approximation's interactions with the lunar pole environment. A, B, C, and D correspond to β angles at 90 deg increments starting with A = 0 deg Figure Legend:

8. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Radiative power distributions across suit segments, 293.72 K (69.02 °F) Figure Legend:

9. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Radiative power distributions with variation in emissivity and radiator temperature Figure Legend:

10. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Suit temperature requirements for constant flux segment dissipation, 300 W Figure Legend:

11. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Emissivity setting requirements for constant flux at a lunar pole at 300 W of constant dissipation Figure Legend:

12. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Emissivity setting requirements for constant flux in lunar pole environment Figure Legend:

13. Date of download: 6/26/2016 Copyright © ASME. All rights reserved. From: Defining a Discretized Space Suit Surface Radiator With Variable Emissivity Properties J. Thermal Sci. Eng. Appl. 2015;7(4):041014-041014-9. doi:10.1115/1.4031132 Allowable total emissivity variations for thermal comfort Figure Legend: