Exoatmospheric calibration sphere

• US 4,527,619 A
• Filed: 07/30/1984
• Issued: 07/09/1985
• Est. Priority Date: 07/30/1984
• Status: Expired due to Fees

• Current Assignee: United States Of America As Represented By The Secretary Of The Army (Government of the United States of America)
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Acker, Roy M., Cartier, Francis R., Stager, David N.
• Primary Examiner(s): DAVIS JR, ALBERT
• Application Number:
  US06/635,854
• Time in Patent Office: 344 Days
• Field of Search: 165/41, 165/104.26, 244/158 R, 244/158 A, 244/159, 244/163
• US Class Current: 165/41
• CPC Class Codes: G01S 7/497 Means for monitoring or calibrating

Abstract

A sphere which provides a high emissivity, uniform, isothermal calibrationource which is fully instrumented for surface temperature and range measurements. The characteristics are achieved by using high thermal conductivity copper hemispheres disposed in spaced, concentric relation and containing a distributed heat pipe therebetween to minimize surface temperature gradients.

Claims

1. A space-based calibration source including support electronics for medium-wave and long-wave infrared sensors having electronics therein for providing range measurements and surface temperature measurements comprising:

a. a pair of spherical members disposed in substantially concentric, spaced relation to form an annular space therebetween; and

b. heat pipe means disposed in said annular space forming an integral, bi-directional structure for minimizing surface temperature gradients on said calibration source.

2. A space-based calibration source as in claim 1 wherein said heat pipe means includes wire wick meshing disposed on the outer surface of said inner sphere and the inner surface of said outer sphere.

3. A space-based calibration source as in claim 2 including a heat pipe working fluid disposed in said annular space.

4. A space-based calibration source as in claim 3 wherein said inner sphere is hermetically sealed.

5. A space-based calibration source as in claim 4 including a pair of support members disposed between each of said spheres for secured relation therebetween, said support members also being covered with said wire wick meshing.

6. A space-based calibration source as in claim 5 including a pair of openings through said spheres to receive a transmitting antenna and a receiving antenna respectively therein.

7. A space-based calibration source as in claim 6 wherein said heat pipe working material is methanol.

8. A space-based calibration source as in claim 7 wherein said spheres are copper.

9. A space-based calibration source as in claim 8 that provides a known surface temperature and range.