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This data has achieved Bronze level on 23 October 2015 which means this data makes a great start at the basics of publishing open data.
Dual Use Catalytically Initiated Combustor (CIC) for Rocket Engine Ignition and Thruster Applications Project
Summary
- Type of release
- a one-off release of a single dataset
- Data Licence
- Not Applicable
- Content Licence
- Creative Commons CCZero
- Verification
- automatically awarded
- Release Date
- 9 April 2015
- Modified Date
- 8 July 2015
- Publishers
- National Aeronautics and Space Administration
- Keywords
- completed, glenn-research-center, project
- Identifier
- dual-use-catalytically-initiated-combustor-cic-for-rocket-engine-ignition-and-thruster-app
- Landing Page
- http://techport.nasa.gov/view/8978
- Maintainers
- TECHPORT SUPPORT hq-techport@mail.nasa.gov
- Language
- en-US
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Description
This proposal responds to subtopic O2.02 "Propulsion Technologies" and the stated need to develop component technologies that will lead to future propulsion systems that are reliable and have adequate performance without requiring excessive specialized handling equipment and procedures or needing to push materials and designs to the limits of their capabilities. We propose the development of a low part count and low energy Catalytically Initiated Combustor (CIC) that can serve as a rocket engine igniter as well as the basis for a family of low cost and highly reliable launch vehicle and satellite thrusters. We propose a 6-month Phase I program to 1) demonstrate reliable ignition and operation of our baseline CIC with hydrogen, methane, and propane fuels, 2) demonstrate reliable ignition and operation of our baseline CIC under cold gas inlet conditions, 3) demonstrate extended duration hot fire testing and durability of our CIC design over multiple ignition cycles, and 4) demonstrate rapid pulsed operation necessary for a launch vehicle or space craft thruster application. Under our proposed Phase I effort, we will also conduct a market survey of potential customers and define a flight weight CIC with maximum commercial utility as either an igniter or small thruster.
General Information
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This data is described at
http://catalog.data.gov/dataset/dual-use-catalytically-initiated-combustor-cic-for-rocket-engine-ignition-and-thruster-app Do you think this data is incorrect? Let us know
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This data is published by
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Legal Information
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The rights statement is at
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Outside the US, this data is available under
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The content is available under
Creative Commons CCZero Do you think this data is incorrect? Let us know
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This data contains
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Practical Information
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The data appears in this collection
http://catalog.data.gov/organization/nasa-gov Do you think this data is incorrect? Let us know
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The accuracy or relevance of this data will
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Technical Information
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This data is published at
http://techport.nasa.gov/xml-api/8978 Do you think this data is incorrect? Let us know
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Find out how to contact someone about this data at
http://catalog.data.gov/dataset/dual-use-catalytically-initiated-combustor-cic-for-rocket-engine-ignition-and-thruster-app Do you think this data is incorrect? Let us know
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Find out how to suggest improvements to publication at
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