WO2014145794A1
|
|
High performance steam cycle
|
WO2014153065A1
|
|
Insulating gas boundary layer for internal combustion engines
|
AU2013273797A1
|
|
Nitrous oxide fuel blend monopropellants
|
WO2013116390A1
|
|
Thermal pressurant
|
WO2013116378A1
|
|
Carbon-on-carbon manufacturing
|
US2014022859A1
|
|
In-tank propellant mixing
|
WO2013103427A2
|
|
Linear detonation wave diverter
|
WO2013033437A2
|
|
Thermal phase separation
|
CN103635669A
|
|
Variable suction exhaust
|
EP2676024A2
|
|
Clustered, fixed cant, throttleable rocket assembly
|
CN103328770A
|
|
High efficiency energy conversion
|
CN102933524A
|
|
Low specific emission decomposition
|
US2011219742A1
|
|
Supersonic combustor rocket nozzle
|
WO2011091162A1
|
|
Insulated combustion chamber
|
AU2010271435A1
|
|
Detonation wave arrestor
|
AU2009324696A1
|
|
Regeneratively cooled porous media jacket
|
EP2209876A1
|
|
Nitrous oxide fuel blend monopropellants
|
EP2092183A2
|
|
Spark-integrated propellant injector head with flashback barrier
|