| http://dbpedia.org/ontology/abstract
|
TM65 is a rocket engine developed by Copenhagen Suborbitals. TM65 uses Ethanol and liquid oxygen as propellants in a pressure-fed power cycle.
, TM65(Tordenskjold 65)は、コペンハーゲン・サブオービタルズによって開発されたHEAT 2X用のロケットエンジンである。TM65は推進剤としてエタノールと液体酸素を使用するガス発生器サイクル(当初は加圧供給式)のロケットエンジンである。
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| http://dbpedia.org/ontology/wikiPageExternalLink
|
https://www.youtube.com/watch%3Fv=bqASqda0ylc&feature=relmfu +
, https://web.archive.org/web/20120516230854/http:/www.copenhagensuborbitals.com/tm65.php +
, http://ing.dk/artikel/128998-count-down-night-i-hab-og-ny-video +
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35799411
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7974
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|
1062862889
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| http://dbpedia.org/ontology/wikiPageWikiLink
|
http://dbpedia.org/resource/Regenerative_cooling_%28rocket%29 +
, http://dbpedia.org/resource/Rocket_engine +
, http://dbpedia.org/resource/Category:Rocket_engines_using_alcohol_propellant +
, http://dbpedia.org/resource/Category:Rocket_engines_using_the_gas-generator_cycle +
, http://dbpedia.org/resource/Ethanol +
, http://dbpedia.org/resource/Water +
, http://dbpedia.org/resource/HEAT_1X_Tycho_Brahe +
, http://dbpedia.org/resource/Copenhagen_Suborbitals +
, http://dbpedia.org/resource/LOX +
, http://dbpedia.org/resource/Liquid_oxygen +
, http://dbpedia.org/resource/Gas-generator_cycle_%28rocket%29 +
, http://dbpedia.org/resource/Pressure-fed_engine_%28rocket%29 +
, http://dbpedia.org/resource/Nitrogen +
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| http://dbpedia.org/property/burnTime
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100.0
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| http://dbpedia.org/property/combustionChamber
|
L* = 200 cm
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| http://dbpedia.org/property/cycle
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http://dbpedia.org/resource/Gas-generator_cycle_%28rocket%29 +
|
| http://dbpedia.org/property/designer
|
http://dbpedia.org/resource/Copenhagen_Suborbitals +
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| http://dbpedia.org/property/diameter
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chamber 400 mm
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| http://dbpedia.org/property/dryWeight
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75.0
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| http://dbpedia.org/property/fuel
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http://dbpedia.org/resource/Ethanol +
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| http://dbpedia.org/property/length
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total 1700 mm
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| http://dbpedia.org/property/manufacturer
|
Copenhagen Suborbitals
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| http://dbpedia.org/property/mixtureRatio
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75
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| http://dbpedia.org/property/name
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TM65
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| http://dbpedia.org/property/nozzleRatio
|
1
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| http://dbpedia.org/property/oxidiser
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http://dbpedia.org/resource/LOX +
|
| http://dbpedia.org/property/predecessor
|
XLR-3A, XLR-3B
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| http://dbpedia.org/property/purpose
|
lower stage booster
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| http://dbpedia.org/property/status
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In development
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| http://dbpedia.org/property/thrustToWeight
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75
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| http://dbpedia.org/property/type
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liquid
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| http://dbpedia.org/property/usedIn
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Planned use in HEAT 2X launch vehicle
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http://dbpedia.org/resource/Template:Reflist +
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, http://dbpedia.org/resource/Template:Copenhagen_Suborbitals +
, http://dbpedia.org/resource/Template:DNK +
|
| http://purl.org/dc/terms/subject
|
http://dbpedia.org/resource/Category:Rocket_engines_using_the_gas-generator_cycle +
, http://dbpedia.org/resource/Category:Rocket_engines_using_alcohol_propellant +
|
| http://purl.org/linguistics/gold/hypernym
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http://dbpedia.org/resource/Engine +
|
| http://www.w3.org/ns/prov#wasDerivedFrom
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http://en.wikipedia.org/wiki/TM65?oldid=1062862889&ns=0 +
|
| http://xmlns.com/foaf/0.1/isPrimaryTopicOf
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http://en.wikipedia.org/wiki/TM65 +
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http://rdf.freebase.com/ns/m.0jt4z3z +
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, http://dbpedia.org/class/yago/Motor103789946 +
, http://dbpedia.org/class/yago/JetEngine103596285 +
|
| rdfs:comment |
TM65 is a rocket engine developed by Copenhagen Suborbitals. TM65 uses Ethanol and liquid oxygen as propellants in a pressure-fed power cycle.
, TM65(Tordenskjold 65)は、コペンハーゲン・サブオービタルズによって開発されたHEAT 2X用のロケットエンジンである。TM65は推進剤としてエタノールと液体酸素を使用するガス発生器サイクル(当初は加圧供給式)のロケットエンジンである。
|
| rdfs:label |
TM65
|
