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ASTM Selected Technical Papers
Thermal Conductivity Measurements of Insulating Materials at Cryogenic Temperatures
By
P. E. Glaser
P. E. Glaser
1
Section head
,
Arthur D. Little, Inc.
,
Cambridge, Mass.
;
symposium chairman
.
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ISBN-10:
0-8031-6630-3
ISBN:
978-0-8031-6630-1
No. of Pages:
125
Publisher:
ASTM International
Publication date:
1967

Two methods of determining the thermal conductivities of cryogenic insulation systems over a wide range of variables are presented and discussed. Both methods are similar in that thermal-conductivity determinations are made calorimetrically by measuring the boiloff rate of the liquid cryogen in the test section. One method utilizes a modified National Bureau of Standards type of cryostat whose capabilities include variation of the external boundary temperature from 212 to −320 F, while the inner boundary temperature is dependent upon the choice of cryogen. Interstitial pressures can be varied from 10−7 torr to 1 atmos. A second method is provided by a flat-plate calorimeter which consists of two isothermal boundaries, one of which is a warm boundary whose temperature can be varied from −320 to 1500 F. The cold boundary consists of two cryogen reservoirs, the calorimeter reservoir and the guard reservoir, whose temperatures are dependent on the cryogen choice. The effect of residual-gas conduction on the thermal conductivity of the insulation can also be determined, as well as the effect of compressive loads on the insulation. Both devices have measured thermal conductivities in the 10−1 to 10−5 Btu/hr ft deg R region.

1.
Black
I. A.
and
Glaser
P. E.
, “
The Performance of a Double-Guarded Cold-Plate Thermal Conductivity Apparatus
,”
Advances in Cryogenic Engineering
, Vol
9
,
Plenum Press
,
New York
,
1964
.
2.
Kropschot
R. H.
, “
Cryogenic Insulation
,” paper presented at the Cryogenic Conference of the ASHRAE Annual Meeting,
Lake Placid, N. Y.
, June 22–24, 1959.
3.
Cunnington
G. R.
and
Zierman
C. A.
, “
Measurement of Thermal Conductivity of Highly Anisotropic Insulations Using a Flat Plate Apparatus
,” presented at 5th Conference on Thermal Conductivity,
Denver, Colo.
, October, 1965.
4.
Streed
E. R.
,
Cunnington
G. R.
, and
Zierman
C. A.
, title
Paper 65-663
, presented at AIAA Thermophysics Specialist Conference,
Monterey, Calif.
, September, 1965.
5.
Gilcrest
A. S.
and
Fick
J. L.
, “
Thermal Problems Related to the Utilization of Highly Anisotropic Multilayer Insulation Systems
,” presented at AIAA Annual Meeting,
New York, N. Y.
, January, 1964.
6.
Nast
T. C.
and
Coston
R. M.
, “
Investigation of the Gas Flow Within Multilayer Insulations and Its Effect on Cryogenic Space Vehicle Design
,”
AIChE Symposium Series
 0065-8812, Vol
62
, No.
61
,
1966
.
7.
Parmley
R. T.
,
Elgin
D. R.
, and
Coston
R. M.
, “
Shingle Multilayer Insulation for Space Vehicles Using Cryogenic Fluids
,”
Advances in Cryogenic Engineering
, Vol
11
,
Plenum Press
,
New York
,
1966
.
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