Evolvable Cryogenics (eCryo)
Project Introduction
eCryo leverages a multi-Center array of enhanced test facilities and new test rigs to mature cryogenic fluid management technologies that are supportive of future exploration propulsion needs and upgraded versions of the Space Launch System (SLS) - from components to entire systems, at a scale relevant to the envisioned applications. Specifically, eCryo will equip mission designers with the knowledge necessary to extend mission durations and increase mission payload capacity for space exploration systems employing cryogenic fluids.
More »Anticipated Benefits
Demonstrated eCryo technologies will equip mission designers with validated models to predict cryogenic fluid behavior for in-space missions and technologies to extend missions employing cryogenic fluids.
More »Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Glenn Research Center
(GRC)
|
Lead Organization | NASA Center | Cleveland, Ohio |
Ames Research Center
(ARC)
|
Supporting Organization | NASA Center | Moffett Field, California |
|
Goddard Space Flight Center
(GSFC)
|
Supporting Organization | NASA Center | Greenbelt, Maryland |
|
Kennedy Space Center
(KSC)
|
Supporting Organization | NASA Center | Kennedy Space Center, Florida |
|
Marshall Space Flight Center
(MSFC)
|
Supporting Organization | NASA Center | Huntsville, Alabama |
| Co-Funding Partners | Type | Location |
|---|---|---|
| Human Exploration and Operations Mission Directorate (HEOMD) | NASA Mission Directorate |
Primary U.S. Work Locations
-
Alabama
-
Florida
-
Maryland
-
Ohio
Project Closeout
eCryo consisted of a product-based portfolio of CFM technologies managed per the WBS structure under NPR 7120.8, with technical products under WBS 4.0 Technology Development and 5.0 Validation & Test. The products under WBS 4.0 Technology Development included: Development and Validation of Analytical Tools (DVAT), Improved Fundamental Understanding of Super Insulation (IFUSI), Radio Frequency Mass Gauge (RFMG), High Accuracy Delta-P Transducer (HADPT), and Valve Seat Leak Test (VSLT). The products under WBS 5.0 Validation & Test include: Integrated Vehicle Fluids (IVF), Structural Heat Intercept Insulation Vibration Evaluation Rig (SHIIVER), and Large Scale Leakage Fixture (LSLF). Over the six year life of the project, key performance parameters were met in all previously listed technology developments. Technology development for the project culminated with the SHIIVER test which provided a large scale test apparatus to evaluate MLI, vapor cooling, and RFMG technologies.
More »| Closeout Documentation | |
|---|---|
| Closeout Link: https://www.nasa.gov/sites/default/files/atoms/files/ecryo_overview_paper_final.pdf | Visit |
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Glenn Research Center (GRC)
Responsible Program:
- Technology Demonstration Missions
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Technology Maturity (TRL)
| Start: | 4 |
| Current: | 4 |
| Estimated End: | 6 |
Technology Areas
Primary:
- TX01 Propulsion Systems
- TX01.1 Chemical Space Propulsion
- TX01.1.1 Integrated Systems and Ancillary Technologies
Target Destinations
Supported Mission Type
