Close

1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/mtc-m17@80/2006/12.11.17.32
Last Update2006:12.11.17.32.48 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m17@80/2006/12.11.17.32.49
Metadata Last Update2018:06.05.03.44.27 (UTC) administrator
Secondary KeyINPE--PRE/
ISBN978-85-85769-27-7
Citation KeyGouvêaVieiCost:2006:H2HyRo
TitleH2O2/Paraffin hybrid rockets for launching nanosats into LEO
FormatCD-ROM
Year2006
Access Date2024, May 14
Secondary TypePRE CI
Number of Files1
Size277 KiB
2. Context
Author1 Gouvêa, Leonardo Henrique
2 Vieira, Ricardo
3 Costa, Fernando de Souza
Resume Identifier1
2 8JMKD3MGP5W/3C9JJ68
3 8JMKD3MGP5W/3C9JH46
Group1 LCP-INPE-MCT-BR
2 LCP-INPE-MCT-BR
3 LCP-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 leo@lcp.inpe.br
2 rvieira@lcp.inpe.br
3 fernando@lcp.inpe.br
Conference NameBrazilian Congress of Thermal Sciences and Engineering, 11 (ENCIT).
Conference LocationCuritiba, PR
Date5-8 dec.
PublisherABCM
Publisher CityRio de Janeiro, RJ
Book TitleProceedings
Tertiary TypePapers
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
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Keywordsparaffin
H2O2
nanosats
low earth orbit (LEO)
specific impulse
mass distribution
AbstractAbstract. 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.
AreaCOMB
Arrangementurlib.net > LABCP > H2O2/Paraffin hybrid rockets...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://mtc-m16b.sid.inpe.br/ibi/sid.inpe.br/mtc-m17@80/2006/12.11.17.32
zipped data URLhttp://mtc-m16b.sid.inpe.br/zip/sid.inpe.br/mtc-m17@80/2006/12.11.17.32
Languageen
Target Fileparaffin.pdf
User Groupadministrator
ignes
Visibilityshown
5. Allied materials
LinkingTrabalho Vinculado à Tese/Dissertação
Next Higher Units8JMKD3MGPCW/3ET38CH
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.46.07 1
Host Collectionlcp.inpe.br/ignes/2004/02.12.18.39
cptec.inpe.br/walmeida/2003/04.25.17.12
6. Notes
Empty Fieldsarchivingpolicy 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
7. Description control
e-Mail (login)marciana
update 


Close