About: TM65

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TM65 is a rocket engine developed by Copenhagen Suborbitals. TM65 uses Ethanol and liquid oxygen as propellants in a pressure-fed power cycle.

Attributes	Values
rdf:type	software 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	TM65 (ja) TM65 (en)
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. (en) 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。 (ja)
name	TM65 (en)
dcterms:subject	Rocket engines using alcohol propellant Rocket engines using the gas-generator cycle
Wikipage page ID	35799411 (xsd:integer)
Wikipage revision ID	1062862889 (xsd:integer)
Link from a Wikipage to another Wikipage	Nitrogen Copenhagen Suborbitals Gas-generator cycle (rocket) Rocket engines using alcohol propellant Rocket engines using the gas-generator cycle Liquid oxygen Ethanol HEAT 1X Tycho Brahe Regenerative cooling (rocket) Water LOX Rocket engine Pressure-fed engine (rocket)
Link from a Wikipage to an external page	http://ing.dk/artikel/128998-count-down-night-i-hab-og-ny-video https://web.archive.org/web/20120516230854/http:/www.copenhagensuborbitals.com/tm65.php https://www.youtube.com/watch%3Fv=bqASqda0ylc&feature=relmfu
sameAs	TM65 TM65 TM65 TM65 TM65
thrust to weight	75 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:About dbt:Convert dbt:DNK dbt:Infobox_rocket_engine dbt:Reflist dbt:Sub dbt:Sup dbt:Copenhagen_Suborbitals
combustion chamber	L* = 200 cm (en)
cycle	Gas-generator cycle (rocket)
designer	Copenhagen Suborbitals
diameter	chamber 400 mm (en)
fuel	Ethanol
length	total 1700 mm (en)
manufacturer	Copenhagen Suborbitals (en)
mixture ratio	75 (xsd:integer)
oxidiser	LOX
predecessor	XLR-3A, XLR-3B (en)
purpose	lower stage booster (en)
status	In development (en)
type	liquid (en)
used in	Planned use in HEAT 2X launch vehicle (en)
has abstract	TM65 is a rocket engine developed by Copenhagen Suborbitals. TM65 uses Ethanol and liquid oxygen as propellants in a pressure-fed power cycle. (en) 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。 (ja)
burn time	100.0 (second)
dry weight	75.0 (kilogram)
nozzle ratio	1 (xsd:integer)
gold:hypernym	Engine
prov:wasDerivedFrom	wikipedia-en:TM65?oldid=1062862889&ns=0
page length (characters) of wiki page	7974 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:TM65
is foaf:primaryTopic of	wikipedia-en:TM65

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