Curtiss-Wright XLR25 rocket engine

E98047

The Curtiss-Wright XLR25 was an American liquid-fueled rocket engine developed in the 1950s to power high-speed experimental research aircraft such as the Bell X-2.

All labels observed (1)

Label Occurrences
Curtiss-Wright XLR25 rocket engine canonical 1

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Statements (29)

Predicate Object
instanceOf liquid-fueled rocket engine
rocket engine
application manned research aircraft
countryOfOrigin United States of America
surface form: United States
developedInDecade 1950s
developer Curtiss-Wright Corporation
surface form: Curtiss-Wright
era 1950s
fuel alcohol
fuelState liquid
intendedRole research propulsion system
manufacturer Curtiss-Wright Corporation
surface form: Curtiss-Wright
notableFeature throttleable thrust for rocket-powered aircraft
operatedIn high-altitude flight tests
supersonic flight regime
oxidizer liquid oxygen
oxidizerState liquid
propellantType bipropellant
liquid propellant
propulsionCycle pressure-fed cycle
propulsionType chemical rocket
status retired
thrustControl throttleable
usedBy NACA
surface form: National Advisory Committee for Aeronautics

United States Air Force
usedFor aeronautical research
high-speed experimental research aircraft
usedIn Bell X-2
experimental aircraft
usedInProgram NASA X-plane series
surface form: X-2 program

How these facts were elicited

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Bell X-2 powerplant Curtiss-Wright XLR25 rocket engine