About: Thermal rocket

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A thermal rocket is a rocket engine that uses a propellant that is externally heated before being passed through a nozzle to produce thrust, as opposed to being internally heated by a redox (combustion) reaction as in a chemical rocket. Thermal rockets can theoretically give high performance, depending on the fuel used and design specifications, and a great deal of research has gone into a variety of types. However, aside from the simple cold gas thruster and steam rocket, none have proceeded past the testing stage.

Attributes	Values
rdf:type	software geo:SpatialThing yago:WikicatRocketEngines yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:Instrumentality103575240 yago:JetEngine103596285 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:Reaction-propulsionEngine104057435 yago:Rocket104099175 yago:Whole100003553
rdfs:label	Thermal rocket (en)
rdfs:comment	A thermal rocket is a rocket engine that uses a propellant that is externally heated before being passed through a nozzle to produce thrust, as opposed to being internally heated by a redox (combustion) reaction as in a chemical rocket. Thermal rockets can theoretically give high performance, depending on the fuel used and design specifications, and a great deal of research has gone into a variety of types. However, aside from the simple cold gas thruster and steam rocket, none have proceeded past the testing stage. (en)
geo:lat	50.169998 (xsd:float)
geo:long	78.375000 (xsd:float)
dcterms:subject	Rocket engines
Wikipage page ID	31137564 (xsd:integer)
Wikipage revision ID	1084023950 (xsd:integer)
Link from a Wikipage to another Wikipage	Beam-powered propulsion Project Rover Propellant depot Saturn I Saturn V Energy density Boltzmann constant Hydrogen De Laval nozzle Pressure vessel Rocket engines S-II S-IVB Nuclear reactor RD-0410 Mirror N-1 rocket NERVA Monatomic gas Combustion Kevin L.G. Parkin Steam Standard gravity Spacecraft propulsion Laser Cold gas thruster Thrust Space race Nevada Test Site Specific impulse Space Transportation System Water Low Earth orbit Radioisotope rocket Molecular mass Rocket engine Rocket engine nozzle Radioisotope heater unit Thermal velocity Rocket nozzle Upper stage Saturated vapor pressure J-2 (rocket engine) Semipalatinsk Effective exhaust velocity Chemical rocket Concentrating solar power Reaction mass Reduction oxidation Robert Bussard dbr:Pewee_2_rocket dbr:Pewee_rocket
sameAs	Thermal rocket Thermal rocket Thermal rocket Thermal rocket Thermal rocket
dbp:wikiPageUsesTemplate	dbt:Citation_needed dbt:Coord dbt:Main dbt:Reflist
georss:point	50.17 78.375
has abstract	A thermal rocket is a rocket engine that uses a propellant that is externally heated before being passed through a nozzle to produce thrust, as opposed to being internally heated by a redox (combustion) reaction as in a chemical rocket. Thermal rockets can theoretically give high performance, depending on the fuel used and design specifications, and a great deal of research has gone into a variety of types. However, aside from the simple cold gas thruster and steam rocket, none have proceeded past the testing stage. (en)
gold:hypernym	Engine
prov:wasDerivedFrom	wikipedia-en:Thermal_rocket?oldid=1084023950&ns=0
page length (characters) of wiki page	10823 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Thermal_rocket
geo:geometry	POINT(78.375 50.169998168945)
is Link from a Wikipage to another Wikipage of	Beam-powered propulsion Nuclear thermal rocket Glossary of aerospace engineering Steam rocket Laser propulsion In situ resource utilization Rocket propellant Radioisotope rocket Rocket engine
is foaf:primaryTopic of	wikipedia-en:Thermal_rocket

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