Spacecraft Thermal Control Handbook, VolumeI: Fundamentals Technologies

Chapter 13: Thermoelectric Coolers

A. Chuchra,
Swales Aerospace, Beltsville, Maryland.
T. Stevenson,
University of Leicester, Leicester, United Kingdom.

Introduction

Thermoelectric coolers (TECs) are miniature solid-state heat pumps capable of providing localized cooling to devices that require cold temperatures for proper operation. Before 1990, their use was confined to unique situations, generally in laboratories or other engineered environments. Throughout the 1990s, however, thermoelectrically cooled devices became somewhat common in everyday terrestrial and commercial applications. Notable examples include six-pack-sized minirefrigerators for automotive and marine use and night-vision devices. TECs in space have also become relatively common; they cool low noise amplifiers (LNAs), star trackers, and IR (infrared) sensors. Table 13.1 lists spaceborne TECs.

Table 13.1: Survey of Spaceborne TECs

Spacecraft or Mission

Instrument/Component

Institution

Launch

No. of Stages

Parallel TECs

Cold Temp. ( C)

Rejection Temp. ( C)

Net Cooling (Tot.) (W)

Input Power (Tot.) (W)

Satcom K

CLNA

RCA Astro

1985

4

Single

50

15

0.79

8.0

Various

Star tracker

Ball

Many for 2 decades

1

Single

0

20

1.8

1.7

Hubble Space Telescope

STIS

Ball, GSFC

1997

4

Single

?80

20

0.3

17.7

Hubble Space Telescope

NICMOS

Ball, UAZ, GSFC

1997

3

Dual

?73

10

0.25

10.75

3

Dual

?47

5

0.6

2.4

FUSE

Fine error sensor (star sensor)

ComDev, CSA, JHU-APL

1999

2

Single

?32

?10 to 0

2 (typ)
5 (max)

Future missions

Hubble Space Telescope

Advanced camera

Ball, JHU-APL

2003

2

Quad

?35

24

1.0

9

4

Single

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