About: Aerojet M-1

Property	Value
dbo:abstract	The Aerojet M-1 was the largest and most powerful liquid-hydrogen-fueled liquid-fuel rocket engine to be designed and component-tested. It was originally developed during the 1950s by the US Air Force. The M-1 offered a baseline thrust of 6.67 MN (1.5 million lbf) and an immediate growth target of 8 MN (1.8 million lbf). If built, the M-1 would have been larger and more efficient than the famed F-1 that powered the first stage of the Saturn V rocket to the Moon. (en) エアロジェット社のM-1はこれまでに設計、製造された最も巨大で強力な液体水素を燃料とするロケットエンジンである。M-1の原型の推力は667万N (150万lbf)で800万N(180万lbf)まで増強する事を見込んでいた。 M-1は月へ向かったサターンVロケットの1段の動力を司るF-1よりも大きな推力を生み出す。 (ja)
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dbp:caption	M-1 rocket engine specifications (en)
dbp:chamberPressure	1000 (xsd:integer)
dbp:countryOfOrigin	dbr:United_States
dbp:cycle	dbr:Gas-generator_cycle_(rocket)
dbp:diameter	4.28 m (en)
dbp:dryWeight	9068.0
dbp:firstDate	Development abandoned at pre-prototype stage (en)
dbp:fuel	dbr:Liquid_hydrogen
dbp:imageSize	300 (xsd:integer)
dbp:length	7.72 m (en)
dbp:manufacturer	dbr:Aerojet
dbp:name	M-1 (en)
dbp:oxidiser	dbr:LOX
dbp:status	Abandoned in development stage. (en)
dbp:thrust(vac)_	1500000 (xsd:integer)
dbp:thrustToWeight	60 (xsd:integer)
dbp:type	liquid (en)
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rdfs:comment	The Aerojet M-1 was the largest and most powerful liquid-hydrogen-fueled liquid-fuel rocket engine to be designed and component-tested. It was originally developed during the 1950s by the US Air Force. The M-1 offered a baseline thrust of 6.67 MN (1.5 million lbf) and an immediate growth target of 8 MN (1.8 million lbf). If built, the M-1 would have been larger and more efficient than the famed F-1 that powered the first stage of the Saturn V rocket to the Moon. (en) エアロジェット社のM-1はこれまでに設計、製造された最も巨大で強力な液体水素を燃料とするロケットエンジンである。M-1の原型の推力は667万N (150万lbf)で800万N(180万lbf)まで増強する事を見込んでいた。 M-1は月へ向かったサターンVロケットの1段の動力を司るF-1よりも大きな推力を生み出す。 (ja)
rdfs:label	Aerojet M-1 (en) M-1 (ロケットエンジン) (ja)
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