|
gptkbp:instanceOf
|
airbreathing jet engine
|
|
gptkbp:advantage
|
high efficiency at hypersonic speeds
|
|
gptkbp:cannotOperateAt
|
zero velocity
|
|
gptkbp:category
|
aerospace engineering
propulsion technology
|
|
gptkbp:challenge
|
material limitations
thermal management
combustion stability
|
|
gptkbp:combustionType
|
supersonic combustion
|
|
gptkbp:compatibleWith
|
oxidizer tank
|
|
gptkbp:distinctFrom
|
ramjet
|
|
gptkbp:firstTestMatch
|
1960s
|
|
gptkbp:fuelType
|
hydrogen
hydrocarbon
|
|
gptkbp:fullName
|
Supersonic Combustion Ramjet
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Scramjet
|
|
gptkbp:maximumSpeed
|
Mach 9.6 (X-43A)
|
|
gptkbp:notableFor
|
gptkb:Boeing_X-51_Waverider
gptkb:NASA_X-43
|
|
gptkbp:operatesIn
|
hypersonic speeds
|
|
gptkbp:requires
|
high initial speed
|
|
gptkbp:studiedBy
|
gptkb:Chinese_Academy_of_Sciences
gptkb:DARPA
gptkb:NASA
gptkb:Australian_Defence_Science_and_Technology_Group
gptkb:Indian_Defence_Research_and_Development_Organisation
Russian Central Institute of Aviation Motors
|
|
gptkbp:usedIn
|
gptkb:aircraft
missiles
space launch systems
|
|
gptkbp:uses
|
atmospheric oxygen
|
|
gptkbp:bfsParent
|
gptkb:Hypersonic_Missiles
|
|
gptkbp:bfsLayer
|
6
|