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   Express Program - Summary
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The EXPRESS program consists of two separate systems: the EXPRESS rack for pressurized payloads and the EXPRESS pallet for attached payloads. EXPRESS is the acronym for EXpedite The PRocessing of Experiments to Space Station.

EXPRESS Rack
The EXPRESS Rack utilizes an International Standard Payload Rack (ISPR) in conjunction with other equipment to provide quick and simple integration of user equipment into the ISPR. Each EXPRESS rack can accommodate a broad range of payloads that meet standard interface requirements. 

The EXPRESS Rack utilizes the ISPR in conjunction with additional structure and electronic equipment designed to provide simple user equipment interfaces. The EXPRESS rack provides accommodations for middeck lockers and drawers. EXPRESS Rack capabilities are:

  • EXPRESS Rack middeck locations can accommodate 72 pounds of experiment equipment, including container weight 
  • Each drawer position accommodates 64 pounds including the weight of the drawer. 
  • A total of 2 kW of 28 V dc power is provided to the payloads 
  • Each payload position receives up to 500 W 
  • Interfaces include RS422, ethernet, analog, discrete, and video 
  • Air cooling is available at all payload locations 
  • Water cooling is available at two payload locations 
  • Nitrogen supply and waste gas vent will be available for one payload location 

External Payload Capabilities

EXPRESS Pallet
The EXPRESS program consists of two separate systems: the EXPRESS rack for pressurized payloads and the EXPRESS pallet for attached payloads. 

The EXPRESS Pallet provides rapid and simple attachment points for experiment equipment outside the ISS. The EXPRESS Pallet has six robotically replaceable adapters for user equipment. 

The EXPRESS Pallet provides power, command and data transmission. Crew operated robotics also can be used for installation and removal of EXPRESS Pallet user equipment. 

Each EXPRESS Pallet Provides: 

  • Accommodation of external payloads up to 6000 lbs. 
  • Payload volumes of ~1.0 m3 
  • 2.5kW power 
  • Command and data transmission services 
  • Fields of view in the nadir, zenith, ram, wake, and Earth-limb directions. 

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