Summary
A mechanical support system is described for a space-borne helium 3 refrigerator. Measurements of the Young's modulus, tensile strength, creep and thermal conductivity of Kevlar cords at room and liquid nitrogen temperatures are discussed and used to predict the performance of the system. Results of vibration tests of the mechanical support are compared with these predictions.
Details
- Original title: Thermal isolation of large loads at low temperature using Kevlar rope.
- Record ID : 1994-1381
- Languages: English
- Source: Cryogenics - vol. 33 - n. 6
- Publication date: 1993
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Indexing
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Balloon-borne helium-3 cryostat for millimetre ...
- Author(s) : PALUMBO P., AQUILINI E., CARDONI P., BERNARDIS P. de, NINNO A. de, MARTINIS L., MASI S., SCARAMUZZI F.
- Date : 1994/12
- Languages : English
- Source: Cryogenics - vol. 34 - n. 12
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The Archeops cryostat: a dilution refrigerator ...
- Author(s) : MADET K., BENOIT A., GAUTIER B.
- Date : 2002/07/22
- Languages : English
- Source: Proceedings of the nineteenth International Cryogenic Engineering Conference. ICEC 19.
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Spray-on foam insulations for launch vehicle cr...
- Author(s) : FESMIRE J. E., COFFMAN B. E., MENEGHELLI B. J., et al.
- Date : 2012/04
- Languages : English
- Source: Cryogenics - vol. 52 - n. 4-6
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Cryotanks in future vehicles.
- Author(s) : HEYDENREICH R.
- Date : 1998/01
- Languages : English
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Fibre composite structures for space applicatio...
- Author(s) : BANSEMIR H., HAIDER O.
- Date : 1998/01
- Languages : English
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