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Autonomous Propellant Loading Project

Metadata Updated: November 12, 2020

The AES Autonomous Propellant Loading (APL) project consists of three activities. The first is to develop software that will automatically control loading of cryogenic propellant into launch vehicles to ensure safe and successful propellant loading.  The second part of the project is to build a system to demonstrate zero-loss cryogenic propellant (liquid hydrogen) transfer and storage, hydrogen liquifaction, and liquid hydrogen densification.  The third area is developing systems to develop technologies to monitor the status of composite tanks used to store cryogenic propellants to ensure they are safe to use.   This project builds on the AES Integrated Ground Operations Demonstration Unit (IGODU) project. The APL project consists of three activities: autonomous control software; demonstrating cryogenic zero-loss transfer and storage, liquifaction, and densification; and developing techniques to monitor composite cryogen storage tanks. As well as being used on Earth, these technologies can be used as part of in situ resource utilization (ISRU), for example to liquify, densify, store, and transfer cryogenic propellants produced on Mars to return astronauts to Earth.

Autonomous Control Software: The autonomous control software contains a physics-based model of the expected system operation. If the inputs from sensors do not agree with the expected system state, the software will determine and initiate the appropriate steps needed to either keep the system operating safely or shut it down safely. This allows the software to perform reasoning based on sensor inputs to determine the causes of anomalies and take appropriate actions. These actions may include reconfiguring the system or safely shutting it down. Initially, the software will be tested using the Universal Propellant Servicing System (UPSS), a small launch vehicle facility being built at Kennedy Space Center (KSC). Once demonstrated on UPSS, the technology is anticipated to be infused into the Space Launch System (SLS) vehicle.

Ground Operations Demonstration Unit for Liquid Hydrogen (GODU LH2) During the Space Shuttle program, engineers at KSC discovered that over 50% of the LH2 purchased by NASA was lost from the time it was loaded onto a tanker, offloaded into a storage container at KSC, transferred from the storage container to the Space Shuttle External Tank and the Space Shuttle launched. This part of APL is to eliminate the losses and enhance liquid hydrogen production and storage by:

Demonstrate zero-loss transfer of LH2 during tanker offload, which has the potential to reduce future SLS LH2 procurement costs by at least 25% Demonstrate in-situ liquefaction of LH2 Demonstrate densification of LH2, which has the potential to improve overall launch vehicle ascent performance by 10% or more.

Tank Health Monitoring (THM) NASA's future goal of exploring the solar system by traveling beyond low Earth orbit with human missions requires new technologies to reduce weight. One technology being investigated for both structural members and propellant tanks is carbon composites. To ensure safety, the failure modes of tanks must be understood. Health monitoring technology is being developed for both structural members and propellant tanks to understand the mechanics and provide a detection system to prevent unexpected catastrophic failure. The overall goal of the project is to test composite tanks under cryogenic temperatures to failure in order to develop health monitoring technology that will detect system degradation and mitigate catastrophic failures through i

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Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

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Dates

Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020

Metadata Source

Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date November 12, 2020
Metadata Updated Date November 12, 2020
Publisher Space Technology Mission Directorate
Unique Identifier Unknown
Maintainer
Identifier TECHPORT_32948
Data First Published 2016-09-01
Data Last Modified 2020-01-29
Public Access Level public
Bureau Code 026:00
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Metadata Catalog ID https://data.nasa.gov/data.json
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Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
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Harvest Source Id 58f92550-7a01-4f00-b1b2-8dc953bd598f
Harvest Source Title NASA Data.json
Homepage URL https://techport.nasa.gov/view/32948
Program Code 026:027
Source Datajson Identifier True
Source Hash 857be53f5e1876c2f838feb77ffe9e6e19c5ce90
Source Schema Version 1.1

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