Project Olympus SAC 2022 Technical Report
This technical report details the design, testing, and manufacturing of a liquid bi-propellant sounding rocket by the Stanford Student Space Initiative for the 2022 Spaceport America Cup’s 30,000ft Hybrid/Liquid Category. The 5 inch diameter, 10 foot long launch vehicle is powered by an N-class nitr...
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| creator | Ali, Rahma Bell, Spencer |
| description | This technical report details the design, testing, and manufacturing of a liquid bi-propellant sounding rocket by the Stanford Student Space Initiative for the 2022 Spaceport America Cup’s 30,000ft Hybrid/Liquid Category. The 5 inch diameter, 10 foot long launch vehicle is powered by an N-class nitrous oxide and kerosene pressure-fed liquid motor with a max. thrust of 350 lbf. Fiberglass structures house custom flight avionics with LoRa radio telemetry capabilities alongside custom parachutes with redundant deployment mechanisms for vehicle recovery. The vehicle will fly a payload studying micro-gravity slosh dynamics to inform future experiments to be performed aboard a Blue Origin launch. |
| doi_str_mv | 10.25740/tx770vm3347 |
| format | Report |
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The vehicle will fly a payload studying micro-gravity slosh dynamics to inform future experiments to be performed aboard a Blue Origin launch.</description><subject>Aerospace engineering</subject><subject>Avionics</subject><subject>FOS: Mechanical engineering</subject><subject>Mechanical engineering</subject><subject>Propulsion systems</subject><subject>Rocket engines</subject><subject>Sloshing (Hydrodynamics)</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>2022</creationdate><recordtype>report</recordtype><sourceid>PQ8</sourceid><recordid>eNpjYBAxNNAzMjU3MdAvqTA3NyjLNTY2Medk0Awoys9KTS5R8M-pzC0oLVYIdnRWMDIwMlIISU3OyMtMTsxRCEotyC8q4WFgTUvMKU7lhdLcDDpuriHOHropiSWJyZklqfEFRZm5iUWV8YYG8WCb4pFsMiZROQCWrDRU</recordid><startdate>2022</startdate><enddate>2022</enddate><creator>Ali, Rahma</creator><creator>Bell, Spencer</creator><general>Stanford Digital Repository</general><scope>DYCCY</scope><scope>PQ8</scope></search><sort><creationdate>2022</creationdate><title>Project Olympus SAC 2022 Technical Report</title><author>Ali, Rahma ; Bell, Spencer</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-datacite_primary_10_25740_tx770vm33473</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Aerospace engineering</topic><topic>Avionics</topic><topic>FOS: Mechanical engineering</topic><topic>Mechanical engineering</topic><topic>Propulsion systems</topic><topic>Rocket engines</topic><topic>Sloshing (Hydrodynamics)</topic><toplevel>online_resources</toplevel><creatorcontrib>Ali, Rahma</creatorcontrib><creatorcontrib>Bell, Spencer</creatorcontrib><collection>DataCite (Open Access)</collection><collection>DataCite</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Ali, Rahma</au><au>Bell, Spencer</au><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Project Olympus SAC 2022 Technical Report</btitle><date>2022</date><risdate>2022</risdate><abstract>This technical report details the design, testing, and manufacturing of a liquid bi-propellant sounding rocket by the Stanford Student Space Initiative for the 2022 Spaceport America Cup’s 30,000ft Hybrid/Liquid Category. 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| identifier | DOI: 10.25740/tx770vm3347 |
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| language | eng |
| recordid | cdi_datacite_primary_10_25740_tx770vm3347 |
| source | DataCite |
| subjects | Aerospace engineering Avionics FOS: Mechanical engineering Mechanical engineering Propulsion systems Rocket engines Sloshing (Hydrodynamics) |
| title | Project Olympus SAC 2022 Technical Report |
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