• DocumentCode
    1746901
  • Title

    Raytheon 95 K high efficiency cryocooler program

  • Author

    Price, Ken D. ; Urbancek, Capt Vladimir

  • Author_Institution
    Raytheon Syst., El Segundo, CA, USA
  • Volume
    5
  • fYear
    2001
  • fDate
    17-17 March 2001
  • Firstpage
    2149
  • Abstract
    Air Force/Raytheon 95K High Efficiency Cryocooler (95 K HEC) Program is developing a new two-stage hybrid Stirling-pulse tube space qualified refrigerator with high heat lift capacity, high efficiency, low weight and size, and low production costs relative to the current state-of-the-art. The basic program will deliver a protoflight Stirling-class Thermo Mechanical Unit (TMU) with protoflight radiation hard electronics. The cooler is designed to support 10 W heat lift from a 95 K source to a 300 K sink. Motor power consumption is to be less than 100 W and system power (including electronics) is to be less than 137 W. The cooler is to weigh no more than 6 Kg. The TMU cold head and compressor designs are highly versatile to enable low cost tailoring to meet the needs of a wide variety of applications. The first demonstration of this versatility is a program option to deliver a companion high-capacity 35 K cryocooler. This cooler will also have an aggressive efficiency requirement. The 95K and 35 K TMU will share over 95% of components, resulting in significant production efficiencies. Another result of this high degree of commonality is that each cooler can be powered and controlled by standardized command and control electronics.
  • Keywords
    Stirling engines; compressors; cooling; focal planes; military systems; missiles; optical tracking; refrigeration; space vehicle electronics; target tracking; 95 K; LWIR FPA; ballistic missile defence; compressor design; high efficiency; high efficiency cryocooler program; high heat lift capacity; low production costs; low size; low weight; protoflight radiation hard electronics; space qualified refrigerator; standardized command and control electronics; thermomechanical cold head; two-stage hybrid Stirling-pulse tube; Biomedical optical imaging; Contracts; Cooling; Costs; Infrared detectors; Missiles; Optical noise; Optical sensors; Space heating; Temperature sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2001, IEEE Proceedings.
  • Conference_Location
    Big Sky, MT, USA
  • Print_ISBN
    0-7803-6599-2
  • Type

    conf

  • DOI
    10.1109/AERO.2001.931170
  • Filename
    931170