Subscale Design of an NTP Engine Exhaust Containment System

Metadata Updated: July 17, 2020

In order for NASA to enable safe manned space flight travel to reach destinations such as Mars, and beyond, advance propulsion technologies, like Nuclear Thermal Propulsion (NTP) will be required.[HTML_REMOVED] Ground testing for engine qualification will be required as part of the process for novel NTP rocket engines development.[HTML_REMOVED] Although NTP engines have been tested in the past, methods that were used (open air NTP exhaust) are not acceptable in today[HTML_REMOVED]s regulatory environment.[HTML_REMOVED] Currently, there is not an acceptable ground test method that has been successfully operated and safely demonstrated which could scale up to the power levels anticipated from NTP engines currently under consideration.[HTML_REMOVED] One favorable method is based on a total containment NTP exhaust system concept, which has been documented as a viable option reported by the ARES Corporation on Nuclear Thermal Propulsion Ground Test Facility (2006) concept definition; the total containment option was recommended as one of three possible ground test facility possibilities.[HTML_REMOVED] There is potential opportunity for Stennis Space Center (SSC) to demonstrate operation of a non-nuclear subscale implementation of the total containment concept for a NTP.[HTML_REMOVED] This goal of this project is to develop preliminary design elements and integrated systems for making a proof-of-concept technology demonstrator subscale system for a non-nuclear rocket engine.[HTML_REMOVED] This subscale system would serve as a non-nuclear test bed which could eventually be used to help optimize design, built, and test systems required for operating a safe, environmentally acceptable NTP ground test facility. A total containment NTP exhaust system has been conceptually engineered, however, since this a completely novel approach to address the numerous issues associated with fully containing exhaust from and NTP rocket engine test, to date, no experimental proof-of-concept has been conducted for this innovative technological approach.[HTML_REMOVED][HTML_REMOVED] Therefore, to demonstrate proof-of-concept, this project will develop the preliminary engineering design for a subscale demonstration for a full exhaust containment system.[HTML_REMOVED] To accomplish this, a closed system of ducts and vessels will be used, and liquid oxygen (LOX) will be injected into the hot hydrogen exhaust to convert it into steam, which will then be condensed and stored as liquid water.[HTML_REMOVED] Any particulates present, due to sub-optimal engine operation, will either be caught in a particle trap, or end up in water storage vessels, which will store the water indefinitely until fission products either decay, or are filtered, and ultimately can be safely discharged.[HTML_REMOVED] Gaseous oxygen and any noble gas fission products will then be condensed in a cryogenic heat exchanger and stored in a chilled jacketed Dewar as LOX, and any residual noble gasses, if present, will solidify and can remain stored in the Dewar indefinitely, until the gases have decayed and can safely be released.[HTML_REMOVED] In this way, all possible fission products that could result from an NTP engine ground test would be captured and stored, and subsequently evaluated and assessed for radioactive contamination and handled accordingly, as needed, over an indefinite period of time.The components for this system will incorporate additional design elements that are currently in[HTML_REMOVED]development that will be integrated with the overall design concept. Valuable data collected from these separate design components would then feed into the development cycle of a full scale NTP ground test facility based on outcomes of the subscale concept.[HTML_REMOVED] The subscale technology demonstrator could ultimately serve as a non-nuclear test bed for NTP ground test facility system components and instrumentation, and would prove to be an invaluable resource for use during the design for a full scale NTP ground test facility.[HTML_REMOVED] The goal of the project is to better prepare and align NASA

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

Metadata Source

Harvested from NASA Data.json

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Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date July 17, 2020
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_14691
Maintainer
TECHPORT SUPPORT
Maintainer Email
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 691415f3-c9ca-4f2f-881c-0a9103b89a34
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2014-09-01
Homepage URL https://techport.nasa.gov/view/14691
Data Last Modified 2020-01-29
Program Code 026:027
Source Datajson Identifier True
Source Hash cc67effdd42808c89be7df4457e40b85c9163db1
Source Schema Version 1.1

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