JPL Technical Report Server

Update on Technology Development Plan for a Low Temperature Hybrid Mars Ascent Vehicle Concept

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dc.contributor.author Karp, Ashley C.
dc.contributor.author Nakazono, Barry
dc.contributor.author Vaughan, David
dc.contributor.author Story, George
dc.contributor.author Oglesby, Britt
dc.contributor.author Prince, Andrew
dc.date.accessioned 2020-05-13T23:17:21Z
dc.date.available 2020-05-13T23:17:21Z
dc.date.issued 2018-07-09
dc.identifier.citation 2018 AIAA Propulsion and Energy Forum, Cincinnati, Ohio, July 9 - 11, 2018 en_US
dc.identifier.clearanceno 18-3089
dc.identifier.uri http://hdl.handle.net/2014/48432
dc.description.abstract Technology development to mature a hybrid rocket option for a potential Mars Ascent Vehicle has been underway at the Jet Propulsion Laboratory and Marshall Space Flight Center. A conceptual design was completed in 2016 and has been used to determine the motor size for risk reduction development. The task plan for the FY17 testing, actually completed in mid FY18, is discussed. The major achievement of this effort was successful full scale hotfire testing with a representative ambient Earth storable propellant combination: SP7/MON3. A near term plan, through July 2019 is briefly discussed. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2018 en_US
dc.title Update on Technology Development Plan for a Low Temperature Hybrid Mars Ascent Vehicle Concept en_US
dc.type Preprint en_US


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