The design characteristics of the baseline engine configuration of the advanced expander cycle engine are described. Several aspects of engine optimization are considered which directly impact the design of the baseline thrust chamber. Four major areas of the power cycle optimization are emphasized: main turbine arrangement; cycle engine source; high pressure pump design; and boost pump drive
The conceptual design for an improved gas turbine (IGT) powertrain and vehicle was investigated. Cyc...
Evaluation testing of modified hypergolic ignition engine operating on gaseous hydrogen and oxyge
The multifuel stratified charge rotary engine is discussed. A single rotor, 0.7L/40 cu in displaceme...
Engine trade studies and systems analyses leading to a baseline engine selection for advanced expand...
Studies included: selection of boost pump designs for low NPSH operation and generation of associate...
An analytical study evaluating thrust chamber cooling engine cycles and preliminary engine design fo...
The objective of the Space Transportation Booster Engine (STBE) Configuration Study is to contribute...
Advanced electric propulsion system concepts with flywheels for electric vehicles are evaluated and ...
Engine testing, ceramic component fabrication and evaluation, component performance rig testing, and...
The engine operating characteristics were examined. Inlet pressure effects, tank pressurization effe...
The best technology program for a small, economically viable gas turbine engine applicable to the ge...
Undeveloped pump-fed, liquid propellant rocket engine cycles were assessed and evaluated for applica...
Technical work on the design and component testing of a 74.5 kW (100 hp) advanced automotive gas tur...
The orbit transfer vehicle (OTV) engine study provided parametric performance, engine programmatic, ...
In Phase 2 of the Advanced Engine Study, the Failure Modes and Effects Analysis (FMEA) maintenance-d...
The conceptual design for an improved gas turbine (IGT) powertrain and vehicle was investigated. Cyc...
Evaluation testing of modified hypergolic ignition engine operating on gaseous hydrogen and oxyge
The multifuel stratified charge rotary engine is discussed. A single rotor, 0.7L/40 cu in displaceme...
Engine trade studies and systems analyses leading to a baseline engine selection for advanced expand...
Studies included: selection of boost pump designs for low NPSH operation and generation of associate...
An analytical study evaluating thrust chamber cooling engine cycles and preliminary engine design fo...
The objective of the Space Transportation Booster Engine (STBE) Configuration Study is to contribute...
Advanced electric propulsion system concepts with flywheels for electric vehicles are evaluated and ...
Engine testing, ceramic component fabrication and evaluation, component performance rig testing, and...
The engine operating characteristics were examined. Inlet pressure effects, tank pressurization effe...
The best technology program for a small, economically viable gas turbine engine applicable to the ge...
Undeveloped pump-fed, liquid propellant rocket engine cycles were assessed and evaluated for applica...
Technical work on the design and component testing of a 74.5 kW (100 hp) advanced automotive gas tur...
The orbit transfer vehicle (OTV) engine study provided parametric performance, engine programmatic, ...
In Phase 2 of the Advanced Engine Study, the Failure Modes and Effects Analysis (FMEA) maintenance-d...
The conceptual design for an improved gas turbine (IGT) powertrain and vehicle was investigated. Cyc...
Evaluation testing of modified hypergolic ignition engine operating on gaseous hydrogen and oxyge
The multifuel stratified charge rotary engine is discussed. A single rotor, 0.7L/40 cu in displaceme...