| dbo:abstract |
نظام الدفع الكهربائي المتقدم هو نظام الدفع الكهربائي بالطاقة الشمسية للمركبات الفضائية التي يتم تصميمها وتطويرها واختبارها بواسطة ناسا وإيروجيت روكيتدين للقيام بمهام علمية واسعة النطاق والنقل. (ar) Advanced Electric Propulsion System (AEPS) is a solar electric propulsion system for spacecraft that is being designed, developed and tested by NASA and Aerojet Rocketdyne for large-scale science missions and cargo transportation. The first application of the AEPS is to propel the Power and Propulsion Element (PPE) of Gateway, to be launched in 2024. The PPE module is built by MAXAR space solutions in Palo Alto, California. Two identical AEPS engines would consume 25 kW being generated by the roll-out solar array (ROSA) assembly, which can produce over 60 kW of power. The Power and Propulsion Element (PPE) for the Lunar Gateway will have a mass of 8-9 metric tons and will be capable of generating 50 kW of solar electric power for its Hall thrusters for maneuverability, which can be supported by chemical monopropellant thrusters for high-thrust attitude control maneuvers. (en) |
| dbo:wikiPageID |
58011682 (xsd:integer) |
| dbo:wikiPageLength |
11049 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
1099457488 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Power_and_Propulsion_Element dbr:Maxar_Technologies dbr:Electric_field dbr:NASA dbr:Lunar_Gateway dbr:Hall-effect_thruster dbr:Asteroid_Redirect_Mission dbr:Propellant dbr:Solar_electric_propulsion dbr:Astronomical_unit dbc:Spacecraft_propulsion dbr:Aerojet_Rocketdyne dbc:Hall_effect dbc:Ion_engines dbc:Lunar_Gateway dbc:Magnetic_propulsion_devices dbr:Jet_Propulsion_Laboratory dbr:Thrust dbr:Newton_(unit) dbr:Xenon dbr:Specific_impulse dbr:Solar_panels_on_spacecraft dbr:Hall_thruster dbr:NASA_Glenn_Research_Center dbr:Solar_electric_power |
| dbp:wikiPageUsesTemplate |
dbt:Annotated_link dbt:Reflist dbt:Short_description dbt:Snd dbt:Use_American_English dbt:Use_mdy_dates dbt:Spacecraft_propulsion |
| dct:subject |
dbc:Spacecraft_propulsion dbc:Hall_effect dbc:Ion_engines dbc:Lunar_Gateway dbc:Magnetic_propulsion_devices |
| rdfs:comment |
نظام الدفع الكهربائي المتقدم هو نظام الدفع الكهربائي بالطاقة الشمسية للمركبات الفضائية التي يتم تصميمها وتطويرها واختبارها بواسطة ناسا وإيروجيت روكيتدين للقيام بمهام علمية واسعة النطاق والنقل. (ar) Advanced Electric Propulsion System (AEPS) is a solar electric propulsion system for spacecraft that is being designed, developed and tested by NASA and Aerojet Rocketdyne for large-scale science missions and cargo transportation. The first application of the AEPS is to propel the Power and Propulsion Element (PPE) of Gateway, to be launched in 2024. The PPE module is built by MAXAR space solutions in Palo Alto, California. Two identical AEPS engines would consume 25 kW being generated by the roll-out solar array (ROSA) assembly, which can produce over 60 kW of power. (en) |
| rdfs:label |
نظام الدفع الكهربائي المتقدم (ar) Advanced Electric Propulsion System (en) |
| owl:sameAs |
wikidata:Advanced Electric Propulsion System dbpedia-ar:Advanced Electric Propulsion System https://global.dbpedia.org/id/5LGng |
| prov:wasDerivedFrom |
wikipedia-en:Advanced_Electric_Propulsion_System?oldid=1099457488&ns=0 |
| foaf:isPrimaryTopicOf |
wikipedia-en:Advanced_Electric_Propulsion_System |
| is dbo:wikiPageWikiLink of |
dbr:Power_and_Propulsion_Element dbr:NASA_Solar_Technology_Application_Readiness dbr:NEXT_(ion_thruster) dbr:Lunar_Gateway dbr:Hall-effect_thruster dbr:Busek dbr:Ion_thruster dbr:Solar_electric_propulsion |
| is foaf:primaryTopic of |
wikipedia-en:Advanced_Electric_Propulsion_System |