Condensation Module for Heat Transfer
Facility Description
The FBCE Condensation Test Module 1 is also referred to as the Condensation Module – Heat Transfer, or CM-HT. CM-HT investigates condensation phenomena in microgravityThe condition of perceived weightlessness created when an object is in free fall, for example when an object is in orbital motion. Microgravity alters many observable phenomena within the physical and life sciences, allowing scientists to study things in ways not possible on Earth. The International Space Station provides access to a persistent microgravity environment.. It includes temperature and pressure sensors and a water-cooled test section to further understanding of fundamental condensation heat transfer in microgravity. It contains a polycarbonate test section outfitted with 61 thermocouples and four pressure transduces. The test section for the CM-HT is comprised of two polycarbonate pieces held in compression by metallic clamp plates, with a circular cross section polycarbonate flow channel contained by two O-ring seals machined inside the polycarbonate. A brazed stainless-steel tube is located inside the circular flow channel, creating an annular space between the outer tube wall and the inner polycarbonate wall. Test fluid is flowed inside the stainless-steel tube while ITCS cooling water is flowed in the opposite direction through the annular space outside of the condensation tube. The test section for CM-HT is outfitted with 61 thermocouples to measure temperature in both the cooling water and test fluid streams. Four thermocouple probes measure the test fluid and water stream temperatures at the inlet and outlet. An additional 24 thermocouple probes measure the water stream temperature along the test section length. And 33 thermocouples are installed on the brazed tube exterior wall in 11 locations along its length, with three thermocouples spaced radially at each location. Also included in the CM-HT are two pressure transducers to measure test fluid absolute pressure and two pressure transducers to measure water absolute pressure. The CM-HT enclosure consists of eight aluminum panels that encompass all the CM-HT hardware.
Availability:The general availability status of the facility. Please contact the facility manager
ISS Environment:The facility location (internal or external to the ISS.) Internal
Owner:The entity that owns the facility. NASA
Operator/Implementation Partner:The entity or ISS National Lab Implementation Partner that operates the facility.
ZIN Technologies
Developer(s):The entity, or entities, that developed the facility.
NASA Glenn Research Center
Facility Manager:The name of the facility manager and their organization.
Nancy Hall
NASA Glenn Research Center
Manager Email:The facility manager's email address.
nancy.r.hall@nasa.gov
Parent Facility:Any facility that is necessary to operate the facility described on this webpage. i.e., a parent facility is one level higher in the operational hierarachy. FBCE
Child Facility:Facilities that can be operated within the facility described on this webpage.
Sponsoring Space Agency:The government space agency that sponsors investigations that use the facility. NASA
Equipment Category:"The facility's ISS National Lab equipment designation type. Designations include:
1. ISS National Lab Commercial Service Provider (CSP) Facility
2. Support Hardware
3. Capability Capability
Additional Information:Additional resources to learn more about the facility.
FBCE>CM-HT on NASA’s SSRE
Optimizing Heat Exchange Flow in Microgravity
Flow Boiling and Condensation Experiment Flight Hardware Development