RF Breakdown Prevention, Part 2 Product Overview

Abstract

Refrigeration tests were performed on the Sunpower CryoTel CT cryocooler to provide design inputs prior to a contractor s payload critical design review. The primary performance matrix was obtained at cold tip temperatures of 60 K, 65 K, and 70 K at heat loads of 3.75 W and 4.5 W. Forced convective air cooling was used to maintain the cryocooler heat rejection temperature at 45 Degrees C. The cooler required 129.5 W of electrical input power to the thermo-mechanical unit (TMU) to remove 4.5 W from the cold tip at 65 K and 112 W of input power to remove 3.75 W at 65 K. By lowering the heat rejection temperature to 30 Degrees C, the required TMU power consumption to remove 4.5 W and 65 K was reduced to 120.3 W. Independent voltage and current measurements were taken to verify the inputs to the vendor s controller and showed good agreement with the commanded power levels.

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Document Details

Document Type
Technical Report
Publication Date
May 07, 2015
Accession Number
ADA627321

Entities

People

  • James Farrell
  • Jeffrey P. Tate
  • Preston T. Partridge

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Aerospace Industry
  • Airborne
  • Antennas
  • Artificial Satellites
  • Best Practices
  • Birds
  • Communication Systems
  • Corporations
  • Cryocoolers
  • Engineering
  • Governments
  • Jet Propulsion
  • Space Systems
  • Spacecraft
  • Spacecraft Components
  • Standards
  • Systems Engineering

Fields of Study

  • Engineering

Readers

  • Electrical Engineering
  • Thermal Physics or Thermal Science.