Logistics Reduction: Heat Melt Compactor

Metadata Updated: July 17, 2020

The Advanced Exploration Systems (AES) Logistics Reduction (LR) project Heat Melt Compactor (HMC) technology is a waste management technology. Currently, there are no waste management practices that are being implemented in the space environment other than manual compaction of waste into a plastic bag. The current practice[HTML_REMOVED]does not recover critical resources such as water, does not prevent the growth of potentially harmful microbiological pathogens, and provides only limited volume reduction.The primary purpose of the HMC is to reduce the volume and[HTML_REMOVED]microbiologically stabilize the waste. The HMC is a device that compacts and heats the trash. The trash is heated to the point where some of the plastic softens and fills the interstitial voids between non-melted trash. The compacted trash is then cooled, resulting in a dry, relatively solid tile that does not exhibit the spring back of traditional compactors. The shape of the tile is predictable and maximizes the efficiency of storage volume. When the trash is heated, it results in a microbiologically-safe tile that can be safely handled by the crew. The HMC can process both wet and dry trash. The water that is driven off the waste is collected and returned to the Water Recovery System. The tiles have ~10% hydrogen by mass from the plastics, wipes, and residual food and can be used to provide additional radiation shielding in the spacecraft.A full-scale, second-generation (Gen2) HMC has been developed and is being used to finalize operational parameters and identify hardware issues. Gen2 HMC tests will allow development of an eventual ISS flight unit. Several SBIR companies were have been award over the HMC period in related areas of microgravity-compatible condensing heat exchanger designs, trash bag liners to allow hygienic tiles after HMC processing, and general HMC system design.[HTML_REMOVED]Limited Gen2 HMC ground testing began in 2017 but was not completed due to inability to reach desired compaction pressure and vaucuum.[HTML_REMOVED] In FY18 the hardware is being repaired to partially restore its desired capability.[HTML_REMOVED] Testing is planned to investigate the use of the ISS vent system as a possible simplification of product gas treatment.[HTML_REMOVED] Additional ground testing in collaboration with industry is planned for FY19.[HTML_REMOVED][HTML_REMOVED]Development and flight[HTML_REMOVED]of a HMC unit to ISS is planned[HTML_REMOVED]in the early 2020s.[HTML_REMOVED]

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Metadata Created Date August 1, 2018
Metadata Updated Date July 17, 2020

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date July 17, 2020
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_93127
Public Access Level public
Bureau Code 026:00
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Harvest Object Id e3683976-66ee-4f77-9723-c60c5c5f9ff7
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2022-01-01
Homepage URL https://techport.nasa.gov/view/93127
Data Last Modified 2020-01-29
Program Code 026:027
Source Datajson Identifier True
Source Hash 1eb37551ec245c8d0336bab5c52332b6a40423a8
Source Schema Version 1.1

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