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Microclimate Cooling: Microclimate Cooling Subsystem (MCSS)

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Microclimate Cooling Subsystem
  • Mitigates heat stress conditions
  • Compact, lightweight design
  • Utilizes ECS Air Platform
  • Water-glycol based cooling medium

Application:

The Microclimate Cooling Subsystem (MCSS) is a variant of the flight qualified US Army Air Warrior Microclimate Cooling System (MCS). The MCSS consists of two heat exchangers connected to the PCA (Pump Control Assembly) integrated into the aircraft or ground vehicle's Environmental Control System ducts. Cold air flows through the fins of the heat exchangers chilling the pumped water-glycol fluid through the umbilical and into the Microclimate Cooling Garment. This personal cooling system further mitigates heat stress in individuals subjected to elevated temperature or wearing thermally restrictive clothing.

Features:

The MCSS uses a 28 VDC pump/controller assembly that circulates the water-glycol based cooling medium through a heat exchanger, providing approximately 230 watts of system cooling capacity in ambient temperatures as high as 105 deg F. The MCSS accommodates two users each having an umbilical mounted control potentiomer allowing the user to individually select the amount of cooling desired. Between the Microclimate Cooling Garment is a low pull force breakaway connector to facilitate "hands free" emergency egress.

Specifications:    
Cooling Medium Water-Glycol Mix  
Cooling 325 watts @ 125 deg F (52 deg C)
Water Temperature 65 to 68 deg F (18 to 20 deg C)
Water Flow Rate 10 to 12 gph (38 to 45 lph)
Weight
   MCCU Heat Exchanger
   MCG
   CBA
   Pump/Controller
   Umbilical Assy


~1.2 lbs
~2.0 lbs
~0.3 lbs
~6.1 lbs
~0.3 lb per ft

(0.5 kg)
(0.91 kg)
(0.14 kg)
(2.8 kg)
(0.45 kg per m)
Electrical Characteristics

   Voltage
   Power
   Specifications

22 to 30 VDC
2.5 amps @ 28 VDC
MIL-STD-461, MIL-STD-704
Component Ref Numbers
   MCCU Heat Exchanger
   MCG
   CBA
   Pump/Controller
   Umbilical Assy
B44819-1
NSN 8415-01-508-1512 (large)
NSN 1680-01-513-5918
B44820-1
consult factory
   
Operating Environment:  
Temperature 55 to 140 deg F (13 to 60 deg C)
Humidity 95% max @ 140 deg F (60 deg C)
Altitude 0 to 20,000 ft (0 to 6,100 m)
Shock consult factory
Vibration consult factory
Crash Safety 20 g each axis  
     
Non-Operationing Environment:  
Temperature -65 to 160 deg F (-54 to 71 deg C)
     
Product Interfaces:  
Power Cable Connector

Mil-Style D38999/24WD5PN


Product Datasheet - PDF
Microclimate Cooling Subsystem


Microclimate Cooling Products

Helicopter
  Land Based

 


© 2008 Carleton Technologies Inc.
Part of the Cobham Life Support Division
10 Cobham Dr. Orchard Park, NY 14127
Phone: 716.662.0006 · Fax: 716.662.0747