| 词条 | Satélite de Reentrada Atmosférica |
| 释义 |
| name = SARA (Satélite de Reentrada Atmosférica) | names_list = | image = | image_caption = | image_alt = | image_size = | mission_type = | operator = Instituto de Aeronáutica e Espaço | Harvard_designation = | COSPAR_ID = | SATCAT = | website = | mission_duration = | distance_travelled = | orbits_completed = | suborbital_range = 300 km (planned) | suborbital_apogee = 350 km (planned) | spacecraft = | spacecraft_type = | spacecraft_bus = | manufacturer = | launch_mass = | BOL_mass = | landing_mass = | dry_mass = | payload_mass = | dimensions = | power = | launch_date = {{start date|2015|11|13|7=Z}} | launch_rocket = VS-40M | launch_site = Centro de Lançamento da Barreira do Inferno | launch_contractor = | deployment_from = | deployment_date = | entered_service = | disposal_type = | deactivated = | destroyed = Launch failure | last_contact = | recovery_by = | recovery_date = | decay_date = | landing_date = | landing_site =
| programme = | previous_mission = | next_mission = | insignia = | insignia_caption = | insignia_alt = | insignia_size = }}SARA - Satélite de Reentrada Atmosférica is a Brazilian satellite project,[1] with the objective of performing experiments in microgravity environment and returning them to the Earth.[2] SARA SuborbitalSARA Suborbital 1/Operação São LourençoThe proposed flight schedule includes a first sub-orbital test flight (SARA Suborbital 1) in 2014[3][4] using a VS-40 rocket launched from the Centro de Lançamento da Barreira do Inferno (Operação São Lourenço).[4] The predicted apogee is 350 km with a range of 300 km. Time spent in microgravity will be around 8 minutes, after which the satellite will reenter the atmosphere and be recovered at sea, 100 km out from Parnaíba. On 13/11/2015 the launch was attempted, resulting on an explosion of the VS-40M V03 rocket on the pad.[5] SARA Suborbital 2A second suborbital flight was planned (SARA Suborbital 2), to test flight attitude control system and de-orbit engine. ConfigurationThe "Sara suborbital" platform heights 350 kg and is divided into four subsystems:
SARA OrbitalThe orbital version of the satellite will operate in a circular 300 km low earth orbit, during a maximum of 10 days. References{{Portal|Spaceflight}}1. ^{{cite web |url=http://www.iae.cta.br/site/page/view/pt.sara.html |title=Instituto de Aeronáutica e Espaço |publisher=Iae.cta.br |date=2008-12-16 |accessdate=2014-03-08 |deadurl=yes |archiveurl=https://web.archive.org/web/20140101073316/http://www.iae.cta.br/site/page/view/pt.sara.html |archivedate=2014-01-01 |df= }} {{-}}{{Brazil space program}}{{DEFAULTSORT:Satelite de Reentrada Atmosferica}}{{Brazil-spacecraft-stub}}2. ^{{cite web|url=http://www.inicepg.univap.br/cd/INIC_2008/anais/arquivosINIC/INIC0101_01_O.pdf |title=Analise De Estrutura Interna Do Modulo de Experimentos Do Sara Suborbital |publisher=Inicepg.univap.br |accessdate=2014-03-08}} 3. ^{{cite web|url=http://www.iae.cta.br/?action=noticia&id=128 |title=Instituto de Aeronáutica e Espaço |publisher=Iae.cta.br |date= |accessdate=2014-03-08}} 4. ^1 Alcântara sedia encontro que discute atividade espacial no País — Portal Brasil 5. ^http://www.fab.mil.br/noticias/mostra/23713/ESPA%C3%87O%20-%20Projeto%20SARA%20continua,%20afirma%20Diretor%20de%20Ci%C3%AAncia%20e%20Tecnologia%20Aeroespacial 1 : Satellites of Brazil |
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