Pulsejet Engine

GPTKB entity

Properties (54)
Predicate Object
gptkbp:instanceOf Engine
gptkbp:energyEfficiency Low
gptkbp:hasContent Simplicity
Inefficiency
gptkbp:hasHistory Developed in 1920s
Used_in_World_War_II
gptkbp:hasPerformance Variable
gptkbp:hasProductLine Valves
Combustor
Exhaust
Intake
gptkbp:hasRelatedPatent gptkb:Model_Aircraft
Sounding Rockets
Research Vehicles
gptkbp:hasType gptkb:Jet_Engine
https://www.w3.org/2000/01/rdf-schema#label Pulsejet Engine
gptkbp:isCharacterizedBy Simple Design
High Speed Operation
High Thrust-to-Weight Ratio
Low Weight
Limited Thrust Control
No Moving Parts
High Fuel Consumption
Can Be Scaled
Can Be Tuned
Can Be Used for Demonstration Purposes
Can Be Used for Educational Purposes
Can Be Used for Hobby Projects
Can Be Used for Research Purposes
Can Be Used for Various Applications
Can Be Used in Hybrid Systems
Can Be Used in Series
Can Be Used in Various Configurations
High Thermal Stress
Low Altitude Performance
Requires Cooling
Short Duration Operation
Can_Be_Used_in_Parallel
Continuous_Combustion
gptkbp:isMonitoredBy gptkb:Heinrich_von_Ohain
gptkb:Sir_Frank_Whittle
gptkbp:isRelatedTo gptkb:Turbojet
gptkb:Rocket_Engine
Scramjet
gptkbp:isUsedFor Metal
Composite Materials
gptkbp:isUsedIn Drones
Missiles
Experimental Aircraft
gptkbp:operatesIn Air
gptkbp:produces Thrust
gptkbp:requires Fuel
gptkbp:trimLevels High
gptkbp:uses Combustion