| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3EsN |
| Repository | sid.inpe.br/iris@1905/2005/08.03.22.37 (restricted access) |
| Last Update | 2018:01.02.11.40.23 (UTC) marciana |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.03.22.37.26 |
| Metadata Last Update | 2021:02.11.18.09.52 (UTC) administrator |
| Secondary Key | INPE-9236-PRE/4908 |
| Label | 10158 |
| Citation Key | PradoViei:2002:OrMaUs |
| Title | Orbital maneuvers using gravitational capture  |
| Format | ISBN:85-900351-3-1 |
| Year | 2002 |
| Secondary Date | 20020511 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LN |
| Number of Files | 1 |
| Size | 299 KiB |
| 2. Context | |
| Author | 1 Prado, Antonio fernando Bertachini de Almeida 2 Vieira, Ernesto |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Balthazar, José Manoel Gonçalves, Paulo Batista Brasil, Reyolando M. F. L. R. F. . |
| Book Title | Nonlinear dynamics, chaos, control and their applications to engineering sciences |
| Publisher | ABCM;SBMAC |
| Pages | cap. 8, 109-128 |
| Series Title | Nonlinear dynamics, chaos, control and their applications to engineering sciences |
| History (UTC) | 2014-09-29 15:09:01 :: administrator -> marciana :: 2002 2018-01-02 11:40:23 :: marciana -> administrator :: 2002 2021-02-11 18:09:52 :: administrator -> :: 2002 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Content Type | External Contribution |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL gravitational capture three-body problem |
| Abstract | The objective of this paper is to study the problem of gravitational capture in the regularized restricted three-body problem. A gravitational capture occurs when a massless particle changes its two-body energy around one celestial body from positive to negative without the use of non-gravitational forces. We studied the importance of several of the parameters involved for a capture in the Earth -Moon system, including the time required for the capture and the effects of the periapse distance. Then, we generalize those results for other binary systems, like the Sun-Earth, Sun-Mars and Sun-Jupiter systems. Next, we cover the whole interval of the mass parameter micro (the mass ratio of the two primaries)and we study the gravitational capture in the interval 0.0 < micro< 0.5. The elliptical restricted problem is also considered as an option for the model. |
| Area | ETES |
| Arrangement | urlib.net > DIDMC > Orbital maneuvers using... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| Target File | 9236.pdf |
| User Group | administrator |
| Visibility | shown |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Host Collection | sid.inpe.br/banon/2001/04.03.15.36 |
| 6. Notes | |
| Empty Fields | affiliation archivingpolicy archivist callnumber city copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |