1. Identity statement | |
Reference Type | Conference Paper (Conference Proceedings) |
Site | mtc-m16b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Repository | sid.inpe.br/mtc-m17@80/2006/12.11.17.32 |
Last Update | 2006:12.11.17.32.48 (UTC) administrator |
Metadata Repository | sid.inpe.br/mtc-m17@80/2006/12.11.17.32.49 |
Metadata Last Update | 2018:06.05.03.44.27 (UTC) administrator |
Secondary Key | INPE--PRE/ |
ISBN | 978-85-85769-27-7 |
Citation Key | GouvêaVieiCost:2006:H2HyRo |
Title | H2O2/Paraffin hybrid rockets for launching nanosats into LEO |
Format | CD-ROM |
Year | 2006 |
Access Date | 2024, May 14 |
Secondary Type | PRE CI |
Number of Files | 1 |
Size | 277 KiB |
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2. Context | |
Author | 1 Gouvêa, Leonardo Henrique 2 Vieira, Ricardo 3 Costa, Fernando de Souza |
Resume Identifier | 1 2 8JMKD3MGP5W/3C9JJ68 3 8JMKD3MGP5W/3C9JH46 |
Group | 1 LCP-INPE-MCT-BR 2 LCP-INPE-MCT-BR 3 LCP-INPE-MCT-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) |
Author e-Mail Address | 1 leo@lcp.inpe.br 2 rvieira@lcp.inpe.br 3 fernando@lcp.inpe.br |
Conference Name | Brazilian Congress of Thermal Sciences and Engineering, 11 (ENCIT). |
Conference Location | Curitiba, PR |
Date | 5-8 dec. |
Publisher | ABCM |
Publisher City | Rio de Janeiro, RJ |
Book Title | Proceedings |
Tertiary Type | Papers |
History (UTC) | 2006-12-11 17:32:49 :: ignes -> administrator :: 2012-10-22 21:03:20 :: administrator -> ignes :: 2006 2013-02-20 14:54:14 :: ignes -> administrator :: 2006 2018-06-05 03:44:27 :: administrator -> marciana :: 2006 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Keywords | paraffin H2O2 nanosats low earth orbit (LEO) specific impulse mass distribution |
Abstract | Abstract. The launching of small payloads or nanosats into low Earth orbit (LEO) by hybrid rockets has been considered in the last years. In the present work it is determined the mass distribution of hybrid propulsion systems using H2O2 and solid paraffin as propellants, to place a 20 kg payload into a 300 km circular equatorial orbit. Two cases are considered: a three-stage hybrid rocket with a total characteristic velocity of 9300 m/s, and three stage air-launched rockets with a total characteristic velocity of 8700 m/s. The effects of the O/F ratio, H2O2 concentration and paraffin composition on specific impulse, thrust coefficient and mass distribution are studied. |
Area | COMB |
Arrangement | urlib.net > LABCP > H2O2/Paraffin hybrid rockets... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | there are no files |
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4. Conditions of access and use | |
data URL | http://mtc-m16b.sid.inpe.br/ibi/sid.inpe.br/mtc-m17@80/2006/12.11.17.32 |
zipped data URL | http://mtc-m16b.sid.inpe.br/zip/sid.inpe.br/mtc-m17@80/2006/12.11.17.32 |
Language | en |
Target File | paraffin.pdf |
User Group | administrator ignes |
Visibility | shown |
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5. Allied materials | |
Linking | Trabalho Vinculado à Tese/Dissertação |
Next Higher Units | 8JMKD3MGPCW/3ET38CH |
Citing Item List | sid.inpe.br/mtc-m21/2012/07.13.14.46.07 1 |
Host Collection | lcp.inpe.br/ignes/2004/02.12.18.39 cptec.inpe.br/walmeida/2003/04.25.17.12 |
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6. Notes | |
Empty Fields | archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor identifier issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject type url versiontype volume |
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7. Description control | |
e-Mail (login) | marciana |
update | |
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