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Products / Blackbodies / Medium Temperature Blackbodies / BB1000

Medium Background Blackbody BB1000


   

Aperture diameter at blackbody interface plate
Minimum operating temperature
Maximum operating temperature
Temperature of radiative environment
Case and Sink


Maximum absolute radiometric Temperature
uncertainty for 2.7 to 5.5 mm bandwidth
Spectral Range
Emissivity
Maximum Spatial Spectral non-uniformity
System field of view

Maximum heating rate
Maximum cool time
Stabilization time
Maximum temperature instability
Operating environment Pressure
Maximum case volume
Power requirements

6.4 to 32 mm


400 K

1000 K

80 K to 300 K
Case follows radiative environment and Cold Sink cooled with Liquid Nitrogen
< 0.5K (1s), 400 to 500 K < 1%
of temperature (1s) from 500 to 800 K
2.7 to 5.5 mm
> 0.99
0.8% (1s) flux at 2.7 mm < 800K
300 degrees full angle for circular FOV
15 K/min
800 to 400 K < 8 hours
1 hour
0.3% (1s) flux at 2.7 mm < 800 K
10-6 torr

260 mm square, 380 long


The blackbody BB1000 under consideration is basically an extended area blackbody for medium temperatures (near ambient up to 1000 K), which operates under cryo-vacuum conditions. The BB1000 was designed and manufactured by VEGA International, Inc. for SDL (Utah) under the contract with SDL/USURF, Subcontract C920306. BB1000 specifications (obtained in tests) are presented in Tab.1, in comparison with requirements of the contract.



BB1000 Blackbody Radiator General Concept
In the base of BB1000 radiator design two principal ideas has been placed:
To use the flat bottom for uniform heat removal.
To use the lateral walls with small emissivity for increasing the influence of zone with maximal radiation losses.

However, the usage of a flat bottom leads to decrease of effective emissivity in comparison of inner or outer conical bottom,especially for coating with significant specular component of reflection.

It is well known that covering of V-shaped or rectangular grooves can increase the emissivity of flat surface. But in this case the cardinal problem is an appearance of the temperature gradient along groove depth.

We choose the configuration of lateral walls, similar to one designed by J. Martin and successfully applied to development of blackbodies of low and medium temperature range . The result of choice of walls configuration (inner surface generatrix of BB1000 radiation cavity) is depicted in.


In order to estimate the longitudinal temperature gradient from bottom to bulge of V-groove, we changed concentric groove that has a radius which is significantly greater than linear dimensions of V-groove, on trapezoidal tooth, which is infinitely extended in direction that perpendicular to its section. We also neglected transversal temperature gradient. The results of computation of temperature difference between lower and upper surfaces of V-grooves are presented in Table 2.

V-groove temperature   Temperature difference due to radiative losses
500 K   11 mK
800 K   119 mK
1000 K   301 mK

The numerical investigation of principal dependencies of effective emissivity for developed blackbody was performed by means of Steep3 modeling software, based on the Monte Carlo algorithm. The main uncertainty of calculation of effective emissivity is connected with variations of data emissivity in various reference books and papers. The results of calculation for two different types of graphite and measured spatial bottom temperature non-uniformity are shown in Fig.2 and are located within 0.9907 to 0.9879 range.










BB1000 Blackbody Design

Blackbody BB1000 (see its schematic drawing in Fig.3) consists of the following elements:
Radiator, formed by the graphite bottom with V-grooves and cold-plated reflector.
Graphite bottom is equipped with two heaters.
The bottom heaters are located on the bottom of a stainless steel cylinder,
which is inserted inside graphite bottom.
The additional heaters are located on the cylinder surface of the
graphite bottom cup for minimize the bottom thermal gradients.
Bottom is equipped with main and additional PRT-100 sensors. Each sensor has the backup one.
Heat exchanger with copper cryogen circulator, which is mechanically coupled with BB reflector.
Multi-foil Ni high-temperature insulation.
Multi-foil Al low-temperature insulation.
Blackbody cavity is attached by the cold reflector to
the Aperture Unit via intermediate stainless steel flange.
Blackbody shroud can be attached to the external shroud of the Aperture Unit.