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- Resistojet_rocket abstract "A resistojet is a method of spacecraft propulsion (electric propulsion) that provides thrust by heating a (typically non-reactive) fluid. Heating is usually achieved by sending electricity through a resistor consisting of a hot incandescent filament, with the expanded gas expelled through a conventional nozzle.Resistojets have been flown in space since 1965 on board military Vela satellites, however they became used in commercial applications in 1980 with launch of first satellites in the INTELSAT-V program. Nowadays resistojet propulsion is used for orbit insertion, attitude control, and deorbit of LEO satellites, including satellites in the Iridium satellite constellation and do well in situations where energy is much more plentiful than mass, and where propulsion efficiency needs to be reasonably high but low thrust is acceptable.[citation needed]".
- Resistojet_rocket wikiPageExternalLink PV2005_4260.pdf.
- Resistojet_rocket wikiPageExternalLink index.php?page=resistojet.
- Resistojet_rocket wikiPageExternalLink SEMNEYAOE1G_UnitedKingdom_0.html.
- Resistojet_rocket wikiPageID "37835".
- Resistojet_rocket wikiPageRevisionID "560651860".
- Resistojet_rocket hasPhotoCollection Resistojet_rocket.
- Resistojet_rocket subject Category:Spacecraft_propulsion.
- Resistojet_rocket comment "A resistojet is a method of spacecraft propulsion (electric propulsion) that provides thrust by heating a (typically non-reactive) fluid.".
- Resistojet_rocket label "Resistojet rocket".
- Resistojet_rocket label "Résistojet".
- Resistojet_rocket sameAs Résistojet.
- Resistojet_rocket sameAs 전기_저항_제트_엔진.
- Resistojet_rocket sameAs m.09flb.
- Resistojet_rocket sameAs Q7315642.
- Resistojet_rocket sameAs Q7315642.
- Resistojet_rocket wasDerivedFrom Resistojet_rocket?oldid=560651860.
- Resistojet_rocket isPrimaryTopicOf Resistojet_rocket.