Nitrous Ethane-Ethylene Rocket with Hypergolic Ignition, Phase I

Metadata Updated: July 17, 2020

The Nitrous Ethane-Ethylene Rocket with Hypergolic Ignition (NEERHI) engine is a proposed technology designed to provide small spacecraft with non-toxic, non-cryogenic, high performance, hypergolic propulsion. When passed over a warm ruthenium catalyst bed, gaseous nitrous oxide and an ethylene-ethane gaseous blend combust instantly. A small 1 N thruster can be designed to provide small satellite propulsion systems with a specific impulse of approximately 300 seconds. Both propellants are self-pressurizing, capable of delivering feed line pressures in excess of 800 psi at room temperature, and 400 psi if cooled to 0?C. For longer duration missions, both nitrous oxide and an ethane-ethylene fuel blend do not require thermal heating to maintain a liquid state, and as such, can be stored on Earth or in space for in-definite periods of time with no parasitic power drain required to maintain a liquid propellant. Compared to other available chemical propulsion systems, a NEERHI system offers a cost effective solution as other hypergolic engines use hydrazine and nitrogen tetroxide which are toxic and dangerous to handle, increasing ground costs. As an added capability, the NEERHI engine has the ability to operate as a monopropellant engine if the ruthenium catalyst be is heated with a bipropellant reaction, increasing the lifetime of the catalyst bed and reducing heating loads on the engine.

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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 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_34041
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 68a70dd5-0e02-4f03-bb90-c92ab07b4c1b
Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2015-12-01
Homepage URL https://techport.nasa.gov/view/34041
Data Last Modified 2020-01-29
Program Code 026:027
Source Datajson Identifier True
Source Hash 36d011dc9fa60aca54057c21843ce9eb7439c5e5
Source Schema Version 1.1

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