| 1. Identity statement | ||||
| Reference Type | Journal Article | |||
| Site | mtc-m21c.sid.inpe.br | |||
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identifier | 8JMKD3MGP3W34R/3RJMHK5 | |||
| Repository | sid.inpe.br/mtc-m21c/2018/08.06.15.23 (restricted access) | |||
| Last Update | 2019:01.10.16.19.34 (UTC) administrator | |||
| Metadata Repository | sid.inpe.br/mtc-m21c/2018/08.06.15.23.48 | |||
| Metadata Last Update | 2021:02.11.18.10.43 (UTC) administrator | |||
| ISSN | 0065-3438. | |||
| Citation Key | MurciaPinerosPrad:2018:ImAeAs | |||
| Title | Impulsive aero-gravity assisted maneuvers in Venus and Mars to change the inclination of a spacecraft  | |||
| Year | 2018 | |||
| Access Date | 2024, May 08 | |||
| Type of Work | conference paper | |||
| Secondary Type | PRE PI | |||
| Number of Files | 1 | |||
| Size | 1947 KiB | |||
| 2. Context | ||||
| Author | 1 Murcia Pineros, Jhonathan Orlando 2 Prado, Antonio Fernando Bertachini de Almeida | |||
| Resume Identifier | 1 2 8JMKD3MGP5W/3C9JGJA | |||
| Group | 1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR 2 DIDMC-CGETE-INPE-MCTIC-GOV-BR | |||
| Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) | |||
| Author e-Mail Address | 1 jhonathan.pineros@inpe.br 2 antonio.prado@inpe.br | |||
| Journal | Advances in the Astronautical Sciences | |||
| Volume | 162 | |||
| Pages | 3921-3936 | |||
| History (UTC) | 2018-08-06 15:23:58 :: simone -> administrator :: 2018 2019-01-04 16:57:07 :: administrator -> simone :: 2018 2019-01-07 10:11:40 :: simone -> administrator :: 2018 2021-02-11 18:10:43 :: administrator -> simone :: 2018 | |||
| 3. Content and structure | ||||
| Is the master or a copy? | is the master | |||
| Content Stage | completed | |||
| Transferable | 1 | |||
| Content Type | External Contribution | |||
| Version Type | publisher | |||
| Abstract | The impulsive or powered aero-gravity-assisted is an orbital maneuver that combines three basic components: A gravity-assisted with a passage by the atmosphere of the planet during the close approach and the application of an impulse during this passage. The mathematical model used to simulate the trajectories is the Restricted Three-Body Problem including aerodynamic forces. The present paper uses this type of maneuver considering atmospheric drag and lift forces. The lift is applied orthogonal to the initial orbital plane to generate an inclination change in the trajectory of the spacecraft, which are very expensive maneuvers. The lift to drag ratio selected goes up to 9.0, because there are vehicles, like waveriders, designed to have these values. When the spacecraft is located at the periapsis the impulse is applied to increase or decrease the variation of energy given by the aero-gravity-assisted maneuver. The planets Venus and Mars are selected to be the secondary bodies for the maneuver, due to their atmospheric density and strategic location to provide possible use for future missions in the solar system. Results of the numerical simulations show the maximum changes in the inclination obtained by the maneuvers as a function of approach angle and direction of the impulse, lift to drag ratio and ballistic coefficient. In the case of Mars, inclination change can be larger than 13°, and for Venus higher than 21°. The energy and inclination variations are shown for several selected orbits. | |||
| Area | ETES | |||
| Arrangement 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Impulsive aero-gravity assisted... | |||
| Arrangement 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Impulsive aero-gravity assisted... | |||
| doc Directory Content | access | |||
| source Directory Content | there are no files | |||
| agreement Directory Content |
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| 4. Conditions of access and use | ||||
| Language | en | |||
| Target File | AAS 17-752.pdf | |||
| User Group | self-uploading-INPE-MCTI-GOV-BR simone | |||
| Visibility | shown | |||
| Read Permission | deny from all and allow from 150.163 | |||
| Update Permission | not transferred | |||
| 5. Allied materials | ||||
| Linking | Trabalho não Vinculado à Tese/Dissertação | |||
| Next Higher Units | 8JMKD3MGPCW/3F2UALS 8JMKD3MGPCW/446AF4B | |||
| Dissemination | WEBSCI; PORTALCAPES; MGA; COMPENDEX. | |||
| Host Collection | urlib.net/www/2017/11.22.19.04 | |||
| 6. Notes | ||||
| Notes | AAS/AIAA Astrodynamics Specialist Conference, 2017; Stevenson; United States; 20 August 2017 through 24 August 2017. | |||
| Empty Fields | alternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress format isbn keywords label lineage mark mirrorrepository month nextedition number orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarytype url | |||
| 7. Description control | ||||
| e-Mail (login) | simone | |||
| update | ||||