Active cooling plans

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Active Coolers for cooling Infrared Detector on satellite payloads

Stirling Cooler

Presentation By

Milind B Naik

TIFR, MUMBAI

Types of coolers

• Passive Coolers

• Radiators

• Stored Cryogens

• Active Coolers

Stirling cycle (this presentation covers this cooler )

• Pulse tube

• Joule-Thompson

• Brayton

• Adiabatic Demagnetization

• 3He coolers

• Optical cooling

• Peltier effect coolers

• Passive Coolers

• Radiators

– Radiators are panels radiating heat according to Stefan's Law

– extremely high reliability

– low mass and a lifetime limited only by surface contamination and degradation

– limitations on the heat load and temperature (typically in the milliwatt range at 70K )

– Multiple stages are often used

• Stored cryogens .

– Dewars containing a cryogen such as liquid helium or solid neon

– excellent temperature stability with no exported vibrations

– substantially increases the launch mass of the vehicle

– limit the lifetime of the mission to the amount of cryogen stored

• Active Coolers

• Stirling cycle .

– These coolers are based on causing a working gas to undergo a Stirling cycle which consists of 2 constant volume processes and two isothermal processes.

– Devices consist of a compressor pump and a displacer unit with a regenerative heat exchanger, known as a `regenerator'.

– Stirling cycle coolers were the first active cooler to be used successfully in space and have proved to be reliable and efficient.

– Recent years have seen the development of two-stage devices which extend the lower temperature range from 60-80K to 15-

30K.

Advantages/disadvantages of different types of cooler technology

Some examples of missions using active coolers

•Missions are listed as vehicle/instrument.

•Design lifetime has been quoted if the instrument is yet to be launched or failed due to another component.

•Excluding electronics.

•STS/BETSE was a technology demonstrator.

•UARS/ISAMS figures per cooler running at 83% stroke.

example of missions using active coolers

Typical cryocooler to be used for satellite payload

MOTOR

COLD FINGER

RICOR

( ISRAEL)

Set of cold-finger available for Cryocooler

Working of stirling cryocooler

Hot side (with heat sink) Cold side (cold finger)

Hot side

Cold side (cold finger)

Working of stirling cryocooler

Test-dewar for cryocooler testing

Cryocooler

Test-dewar

Test-dewar for cryocooler testing

Temperature Sensor

Vacuum

• Various processes involved for testing

Stirling cryocooler

– Design, development of test-dewar with vacuum seal, feedthrough wires, optical window, temperature sensor integration with cold-finger etc.

– Assembly , evacuation of test-dewarCrcycooler assembly

– Crycooler Fill and purge with Helium

– Various leak tests

– Functional tests

– Calibrations

– Others.

Thanks …

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