Assuming that the droplet layer is a uniform medium, an evaporation intensity analogous to radiation intensity was defined based on an analysis of vapor molecule transfer characteristics in the droplet layer. An evaporation transfer equation was then established, from which a one-dimensional evaporative mass flux expression was obtained and combined with the radiation heat transfer model. The combined radiation-evaporation model was used to analyze the influence of the exit temperature and the optical thickness of the droplet layer on temperature distribution, evaporation loss rate, and system lifetime. In the case of a certain droplet diameter and a small optical thickness (κD1), the numerical results show that temperature decreases approximately linearly with layer length. The evaporation loss rate increases as the exit temperature and optical thickness increase, and the main contribution to the evaporation loss rate comes from the high temperature portion of the liquid layer near the exit of the liquid generator, i.e., the evaporation loss rate increases rapidly in a short length of the liquid droplet layer and approaches a stable value as the length reaches a certain value. With the same working fluid mass overloading proportion of the droplet layer, the system lifetime is mainly determined by the exit temperature of the liquid droplet layer. For example, if the exit temperature decreases from 320 to 310 K, the system lifetime increases by approximately three times. However, system lifetime has a weak relationship with optical thickness.

References

1.
Saadon
,
S.
, and
Sidek
,
O.
, 2011, “
A Review of Vibration-Based MEMS Piezoelectric Energy Harvesters
,”
Energy Convers. Manage.
,
52
(
1
), pp.
500
504
.
2.
Biter
,
W.
,
Hess
,
S.
, and
Sung
,
O.
, 2006, “
Development Status of Electrostatic Switched Radiator
,”
AIP Conf. Proc.
,
813
,
56
63
.
3.
Totani
,
T.
,
Kodama
,
T.
,
Nagata
,
H.
, and
Kudo
,
I.
, 2005, “
Thermal Design of Liquid Droplet Radiator for Space Solar-Power System
,”
J. Spacecr. Rockets
,
42
(
3
), pp.
493
499
.
4.
Hung
,
Y. M.
, and
Seng
,
Q.
, 2011, “
Effects of Geometric Design on Thermal Performance of Star-Groove Micro-Heat Pipes
,”
Int. J. Heat Mass Transfer
,
54
(
5–6
), pp.
1198
1209
.
5.
Demiryont
,
H.
, and
Moorehead
,
D.
, 2009, “
Electrochromic Emissivity Modulator for Spacecraft Thermal Management
,”
Sol. Energy Mater. Sol. Cells
,
93
(
12
), pp.
2075
2078
.
6.
Demiryont
,
H.
,
Shannon
,
K. C.
, and
Sheets
,
J.
, 2009, “
Emissivity Modulating Electrochromic Device
,”
Proc. SPIE
7331
, p.
73310I
.
7.
Pfeiffer
,
S. L.
, 1989, “
Concepture Design of Liquid Droplet Radiator Shuttle–Attached Experiment
,” NASA Contract Report No. 185165.
8.
Totani
,
T.
,
Itami
,
M.
,
Nagata
,
H.
,
Kudo
,
I.
, and
Iwasaki
,
A.
, 2004, “
Measurement Technique for Pumping Performance of a Centrifugal Collector Under Microgravity
,”
Rev. Sci. Instrum.
,
75
(
2
), pp.
515
523
.
9.
Totani
,
T.
,
Kodama
,
T.
,
Watanabe
,
K.
,
Nanbu
,
K.
,
Nagata
,
H.
, and
Kudo
,
I.
, 2006, “
Numerical and Experimental Studies on Circulation of Working Fluid in Liquid Droplet Radiator
,”
Acta Astronaut.
,
59
(
1–5
), pp.
192
199
.
10.
Siegel
,
R.
, 1987, “
Transient Radiative Cooling of a Droplet-Filled Layer
,”
J. Heat Transfer
,
109
(
1
), pp.
159
164
.
11.
Siegel
,
R.
, 1989, “
Radiative Cooling Performance of a Converging Liquid Drop Radiator
,”
J. Thermophys. Heat Transfer
,
3
(
1
), pp.
46
52
.
12.
Siegel
,
R.
, 1989, “
Transient Radiative Cooling of an Absorbing and Scattering Cylinder
,”
J. Heat Transfer
,
111
(
1
), pp.
199
203
.
13.
Brown
,
R. F.
, and
Kosson
,
R.
, 1984, “
Liquid Droplet Radiator Sheet Design Considerations
,”
19th Intersociety Energy Conversion Engineering Conference
,
American Nuclear Society
,
La Grange Park, Illionis
, Vol.
1
, pp.
330
338
, Paper No. 849304.
14.
Chen
,
P. J.
, 1987,
Scientific Foundation of Vacuum Technology
,
National Defense Industry Press
,
Beijing
, Chap. II, pp.
92
93
, Chap. V, pp. 233–234.
15.
Chubb
,
D. L.
,
Calfo
,
F. D.
, and
McMaster
,
M. S.
, 1993, “
Current Status of Liquid Sheet Radiator Research
,” NASA Technical Memorandum No.105764.
16.
Yu
,
Q. Z.
, 2000,
Radiation Heat Transfer Principle
,
Harbin Institute of Technology Press
,
Harbin
, Chap. XII, pp.
161
164
, 172–173.
17.
Hertzberg
,
A.
, 1988, “
Basic and Applied Research Related to the Technology of Space Energy Conversion Systems
,”
Semi-Annual Report
, NASA Grant NAG 1-327,
University of Washington
,
Seattle
.
You do not currently have access to this content.