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- Dual_mode_propulsion_rocket abstract "Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets. Dual mode systems are either hydrazine/N2O4, or MMH/hydrogen peroxide (the former is much more common). Typically, this system works as follows: During the initial high-impulse orbit-raising maneuvers, the system operates in a bipropellant fashion, providing high thrust at high efficiency; when it arrives on orbit, it closes off either the fuel or oxidizer, and conducts the remainder of its mission in a simple, predictable monopropellantfashion.".
- Dual_mode_propulsion_rocket wikiPageID "37834".
- Dual_mode_propulsion_rocket wikiPageLength "922".
- Dual_mode_propulsion_rocket wikiPageOutDegree "13".
- Dual_mode_propulsion_rocket wikiPageRevisionID "493837762".
- Dual_mode_propulsion_rocket wikiPageWikiLink Category:Spacecraft_propulsion.
- Dual_mode_propulsion_rocket wikiPageWikiLink Fuel.
- Dual_mode_propulsion_rocket wikiPageWikiLink Hydrazine.
- Dual_mode_propulsion_rocket wikiPageWikiLink Hydrogen_peroxide.
- Dual_mode_propulsion_rocket wikiPageWikiLink Impulse_(physics).
- Dual_mode_propulsion_rocket wikiPageWikiLink Liquid-propellant_rocket.
- Dual_mode_propulsion_rocket wikiPageWikiLink Monopropellant_rocket.
- Dual_mode_propulsion_rocket wikiPageWikiLink Orbit.
- Dual_mode_propulsion_rocket wikiPageWikiLink Oxidizing_agent.
- Dual_mode_propulsion_rocket wikiPageWikiLink Propulsion.
- Dual_mode_propulsion_rocket wikiPageWikiLink Spacecraft_propulsion.
- Dual_mode_propulsion_rocket wikiPageWikiLink Thrust.
- Dual_mode_propulsion_rocket wikiPageWikiLinkText "Dual mode propulsion rocket".
- Dual_mode_propulsion_rocket wikiPageUsesTemplate Template:Rocket-stub.
- Dual_mode_propulsion_rocket wikiPageUsesTemplate Template:Unreferenced.
- Dual_mode_propulsion_rocket subject Category:Spacecraft_propulsion.
- Dual_mode_propulsion_rocket type Astrodynamic.
- Dual_mode_propulsion_rocket type Technology.
- Dual_mode_propulsion_rocket comment "Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets. Dual mode systems are either hydrazine/N2O4, or MMH/hydrogen peroxide (the former is much more common).".
- Dual_mode_propulsion_rocket label "Dual mode propulsion rocket".
- Dual_mode_propulsion_rocket sameAs Q5310218.
- Dual_mode_propulsion_rocket sameAs m.09fk_.
- Dual_mode_propulsion_rocket sameAs Q5310218.
- Dual_mode_propulsion_rocket wasDerivedFrom Dual_mode_propulsion_rocket?oldid=493837762.
- Dual_mode_propulsion_rocket isPrimaryTopicOf Dual_mode_propulsion_rocket.