| 1. Identity statement | |
| Reference Type | Journal Article |
| Site | mtc-m16.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZsFDuKxG/AuH7L |
| Repository | sid.inpe.br/marciana/2003/12.18.13.17 (restricted access) |
| Last Update | 2004:11.30.02.00.00 (UTC) administrator |
| Metadata Repository | sid.inpe.br/marciana/2003/12.18.13.17.51 |
| Metadata Last Update | 2021:02.11.18.10.16 (UTC) administrator |
| Secondary Key | INPE-11617-PRE/6999 |
| ISSN | 0100-7386 |
| Citation Key | Prado:2003:ElPlTr |
| Title | The Elliptic-Bi-Parabolic Planar Transfer for Artificial Satellites  |
| Year | 2003 |
| Month | abr./jun. |
| Access Date | 2024, Apr. 28 |
| Secondary Type | PRE PN |
| Number of Files | 1 |
| Size | 370 KiB |
| 2. Context | |
| Author | Prado, Antonio Fernando Bertachini de Almeida |
| Resume Identifier | 8JMKD3MGP5W/3C9JGJA |
| Group | DMC-INPE-MCT-BR |
| Journal | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
| Volume | 25 |
| Number | 2 |
| Pages | 122 - 128 |
| History (UTC) | 2005-01-06 10:50:06 :: marciana -> administrator :: 2021-02-11 18:10:16 :: administrator -> marciana :: 2003 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Keywords | Astrodynamics orbital maneuvers swing-by |
| Abstract | The "elliptic-bi-parabolic transfer" orbit for an artificial satellite is an extension of the bi-parabolic transfer that uses a Swing-By with a natural satellite of the main body to reduce the amount of fuel required by the maneuver. The objective is to find the minimum cost trajectory, in terms of fuel consumed, to transfer a spacecraft from a parking orbit around a planet to an orbit around a natural satellite of this planet or to a higher orbit around the planet. Graphics are built to show in more details the potential savings given by this technique. After that, the idea of using a natural satellite in the maneuver is applied to the problem of making a spacecraft to escape from the main planet to the interplanetary space with maximum velocity at infinity. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > The Elliptic-Bi-Parabolic Planar... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| Language | en |
| Target File | script=sci_arttext&pid=S1678-58.pdf |
| User Group | administrator |
| Visibility | shown |
| Copy Holder | SID/SCD |
| Archiving Policy | denypublisher denyfinaldraft |
| Read Permission | deny from all and allow from 150.163 |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Dissemination | WEBSCI; PORTALCAPES. |
| Host Collection | sid.inpe.br/banon/2003/08.15.17.40 |
| 6. Notes | |
| Empty Fields | affiliation alternatejournal archivist callnumber copyright creatorhistory descriptionlevel documentstage doi e-mailaddress electronicmailaddress format isbn label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype |
| 7. Description control | |
| e-Mail (login) | marciana |
| update | |