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- TM65 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 wikiPageExternalLink 128998-count-down-night-i-hab-og-ny-video?utm_source=feed&utm_medium=rss&utm_campaign=rumfartpaadenandenmaade.
- TM65 wikiPageExternalLink tm65.php.
- TM65 wikiPageExternalLink watch?v=bqASqda0ylc&feature=relmfu.
- TM65 wikiPageID "35799411".
- TM65 wikiPageRevisionID "585811466".
- TM65 burnTime "100.0".
- TM65 chamberPressure "12.0".
- TM65 combustionChamber "L* = 200 cm".
- TM65 cycle Gas-generator_cycle.
- TM65 designer Copenhagen_Suborbitals.
- TM65 diameter "chamber 400 mm".
- TM65 dryWeight "75.0".
- TM65 fuel Ethanol.
- TM65 hasPhotoCollection TM65.
- TM65 length "total 1700 mm".
- TM65 manufacturer "Copenhagen Suborbitals".
- TM65 mixtureRatio "75".
- TM65 name "TM65".
- TM65 nozzleRatio "1".
- TM65 oxidiser Liquid_oxygen.
- TM65 predecessor "XLR-3A, XLR-3B".
- TM65 purpose "lower stage booster".
- TM65 specificImpulseSeaLevel "200.0".
- TM65 specificImpulseVacuum "230.0".
- TM65 status "In development".
- TM65 thrust(sl)_ "65 kN".
- TM65 thrust(vac)_ "85 kN".
- TM65 thrustToWeight "75".
- TM65 type "liquid".
- TM65 usedIn "Planned use in HEAT 2X launch vehicle".
- TM65 subject Category:Rocket_engines.
- TM65 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 label "TM65".
- TM65 sameAs m.0jt4z3z.
- TM65 sameAs Q7670637.
- TM65 sameAs Q7670637.
- TM65 wasDerivedFrom TM65?oldid=585811466.
- TM65 isPrimaryTopicOf TM65.